Execution Chart

We display below the execution chart for this examination (boot time has been removed).

Trace from the execution

Formatting '/data/fkordon/mcc2023-input.r001-oct2-167813588400246.qcow2', fmt=qcow2 cluster_size=65536 extended_l2=off compression_type=zlib size=4294967296 backing_file=/data/fkordon/mcc2023-input.qcow2 backing_fmt=qcow2 lazy_refcounts=off refcount_bits=16
Waiting for the VM to be ready (probing ssh)
....................
=====================================================================
Generated by BenchKit 2-5348
Executing tool marcie
Input is AirplaneLD-PT-0010, examination is ReachabilityCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r001-oct2-167813588400246
=====================================================================

--------------------
preparation of the directory to be used:
/home/mcc/execution
total 568K
-rw-r--r-- 1 mcc users 12K Feb 26 11:11 CTLCardinality.txt
-rw-r--r-- 1 mcc users 85K Feb 26 11:11 CTLCardinality.xml
-rw-r--r-- 1 mcc users 9.0K Feb 26 11:09 CTLFireability.txt
-rw-r--r-- 1 mcc users 68K Feb 26 11:09 CTLFireability.xml
-rw-r--r-- 1 mcc users 4.2K Jan 29 11:40 GenericPropertiesDefinition.xml
-rw-r--r-- 1 mcc users 6.5K Jan 29 11:40 GenericPropertiesVerdict.xml
-rw-r--r-- 1 mcc users 6.2K Feb 25 15:30 LTLCardinality.txt
-rw-r--r-- 1 mcc users 31K Feb 25 15:30 LTLCardinality.xml
-rw-r--r-- 1 mcc users 4.3K Feb 25 15:30 LTLFireability.txt
-rw-r--r-- 1 mcc users 26K Feb 25 15:30 LTLFireability.xml
-rw-r--r-- 1 mcc users 17K Feb 26 11:14 ReachabilityCardinality.txt
-rw-r--r-- 1 mcc users 99K Feb 26 11:14 ReachabilityCardinality.xml
-rw-r--r-- 1 mcc users 13K Feb 26 11:13 ReachabilityFireability.txt
-rw-r--r-- 1 mcc users 89K Feb 26 11:13 ReachabilityFireability.xml
-rw-r--r-- 1 mcc users 1.8K Feb 25 15:30 UpperBounds.txt
-rw-r--r-- 1 mcc users 3.9K Feb 25 15:30 UpperBounds.xml
-rw-r--r-- 1 mcc users 5 Mar 5 18:22 equiv_col
-rw-r--r-- 1 mcc users 5 Mar 5 18:22 instance
-rw-r--r-- 1 mcc users 6 Mar 5 18:22 iscolored
-rw-r--r-- 1 mcc users 48K Mar 5 18:22 model.pnml

--------------------
content from stdout:

=== Data for post analysis generated by BenchKit (invocation template)

The expected result is a vector of booleans
BOOL_VECTOR

here is the order used to build the result vector(from text file)
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-00
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-01
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-02
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-03
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-04
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-05
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-06
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-07
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-08
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-09
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-10
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-11
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-12
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-13
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-14
FORMULA_NAME AirplaneLD-PT-0010-ReachabilityCardinality-15

=== Now, execution of the tool begins

BK_START 1678388053898

bash -c /home/mcc/BenchKit/BenchKit_head.sh 2> STDERR ; echo ; echo -n "BK_STOP " ; date -u +%s%3N
Invoking MCC driver with
BK_TOOL=marcie
BK_EXAMINATION=ReachabilityCardinality
BK_BIN_PATH=/home/mcc/BenchKit/bin/
BK_TIME_CONFINEMENT=3600
BK_INPUT=AirplaneLD-PT-0010
Not applying reductions.
Model is PT
ReachabilityCardinality PT
timeout --kill-after=10s --signal=SIGINT 1m for testing only

Marcie built on Linux at 2019-11-18.
A model checker for Generalized Stochastic Petri nets

authors: Alex Tovchigrechko (IDD package and CTL model checking)

Martin Schwarick (Symbolic numerical analysis and CSL model checking)

Christian Rohr (Simulative and approximative numerical model checking)

marcie@informatik.tu-cottbus.de

called as: /home/mcc/BenchKit/bin//../marcie/bin/marcie --net-file=model.pnml --mcc-file=ReachabilityCardinality.xml --memory=6 --mcc-mode

parse successfull
net created successfully

Net: AirplaneLD_PT_0010
(NrP: 89 NrTr: 88 NrArc: 333)

parse formulas
formulas created successfully
place and transition orderings generation:0m 0.001sec

net check time: 0m 0.000sec

init dd package: 0m 3.026sec


RS generation: 0m 0.021sec


-> reachability set: #nodes 1379 (1.4e+03) #states 43,463 (4)



starting MCC model checker
--------------------------

checking: EF [95<=stp1]
normalized: E [true U 95<=stp1]

abstracting: (95<=stp1)
states: 0
-> the formula is FALSE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-02 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.001sec

checking: AG [TheAltitude_5<=1]
normalized: ~ [E [true U ~ [TheAltitude_5<=1]]]

abstracting: (TheAltitude_5<=1)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-10 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.000sec

checking: AG [1<=AltitudePossibleVal_4]
normalized: ~ [E [true U ~ [1<=AltitudePossibleVal_4]]]

abstracting: (1<=AltitudePossibleVal_4)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-13 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.000sec

checking: AG [1<=WeightPossibleVal_off]
normalized: ~ [E [true U ~ [1<=WeightPossibleVal_off]]]

abstracting: (1<=WeightPossibleVal_off)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-14 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.000sec

checking: AG [sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=2]
normalized: ~ [E [true U ~ [sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=2]]]

abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=2)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-05 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.022sec

checking: EF [~ [P3<=stp3]]
normalized: E [true U ~ [P3<=stp3]]

abstracting: (P3<=stp3)
states: 41,043 (4)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-07 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.006sec

checking: AG [Speed_Left_Wheel_1<=SpeedPossibleVal_2]
normalized: ~ [E [true U ~ [Speed_Left_Wheel_1<=SpeedPossibleVal_2]]]

abstracting: (Speed_Left_Wheel_1<=SpeedPossibleVal_2)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-15 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.001sec

checking: EF [~ [[1<=AltitudePossibleVal_13 | P5<=TheAltitude_10]]]
normalized: E [true U ~ [[1<=AltitudePossibleVal_13 | P5<=TheAltitude_10]]]

abstracting: (P5<=TheAltitude_10)
states: 43,452 (4)
abstracting: (1<=AltitudePossibleVal_13)
states: 43,463 (4)
-> the formula is FALSE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-09 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.001sec

checking: EF [47<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)]
normalized: E [true U 47<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)]

abstracting: (47<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1))
states: 0
-> the formula is FALSE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-00 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.024sec

checking: AG [~ [[stp3<=30 & 32<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)]]]
normalized: ~ [E [true U [stp3<=30 & 32<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)]]]

abstracting: (32<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 0
abstracting: (stp3<=30)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-04 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.025sec

checking: EF [[[[TheAltitude_5<=1 & [[~ [TheAltitude_14<=AltitudePossibleVal_20] & [[[[1<=Speed_Right_Wheel_2 | TheAltitude_5<=0] & [P1<=0 | Plane_On_Ground_Signal_no_F<=0]] | ~ [SpeedPossibleVal_9<=0]] & [~ [[P3<=AltitudePossibleVal_19 & SpeedPossibleVal_2<=AltitudePossibleVal_13]] & [[1<=AltitudePossibleVal_5 | AltitudePossibleVal_16<=stp4] & [Plane_On_Ground_Signal_no_T<=0 | AltitudePossibleVal_10<=1]]]]] & Speed_Left_Wheel_9<=0]] & [P5<=TheAltitude_10 & AltitudePossibleVal_1<=Weight_Right_Wheel_off]] & AltitudePossibleVal_11<=0]]
normalized: E [true U [[[P5<=TheAltitude_10 & AltitudePossibleVal_1<=Weight_Right_Wheel_off] & [[[[[[[Plane_On_Ground_Signal_no_T<=0 | AltitudePossibleVal_10<=1] & [1<=AltitudePossibleVal_5 | AltitudePossibleVal_16<=stp4]] & ~ [[P3<=AltitudePossibleVal_19 & SpeedPossibleVal_2<=AltitudePossibleVal_13]]] & [~ [SpeedPossibleVal_9<=0] | [[P1<=0 | Plane_On_Ground_Signal_no_F<=0] & [1<=Speed_Right_Wheel_2 | TheAltitude_5<=0]]]] & ~ [TheAltitude_14<=AltitudePossibleVal_20]] & Speed_Left_Wheel_9<=0] & TheAltitude_5<=1]] & AltitudePossibleVal_11<=0]]

abstracting: (AltitudePossibleVal_11<=0)
states: 0
abstracting: (TheAltitude_5<=1)
states: 43,463 (4)
abstracting: (Speed_Left_Wheel_9<=0)
states: 39,514 (4)
abstracting: (TheAltitude_14<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (TheAltitude_5<=0)
states: 41,406 (4)
abstracting: (1<=Speed_Right_Wheel_2)
states: 3,951 (3)
abstracting: (Plane_On_Ground_Signal_no_F<=0)
states: 43,462 (4)
abstracting: (P1<=0)
states: 20,594 (4)
abstracting: (SpeedPossibleVal_9<=0)
states: 0
abstracting: (SpeedPossibleVal_2<=AltitudePossibleVal_13)
states: 43,463 (4)
abstracting: (P3<=AltitudePossibleVal_19)
states: 43,463 (4)
abstracting: (AltitudePossibleVal_16<=stp4)
states: 3,949 (3)
abstracting: (1<=AltitudePossibleVal_5)
states: 43,463 (4)
abstracting: (AltitudePossibleVal_10<=1)
states: 43,463 (4)
abstracting: (Plane_On_Ground_Signal_no_T<=0)
states: 33,166 (4)
abstracting: (AltitudePossibleVal_1<=Weight_Right_Wheel_off)
states: 12,705 (4)
abstracting: (P5<=TheAltitude_10)
states: 43,452 (4)
-> the formula is FALSE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-11 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.007sec

checking: AG [[[[~ [WeightPossibleVal_off<=AltitudePossibleVal_1] | [[[~ [[Weight_Left_Wheel_on<=0 & 1<=TheAltitude_2]] | 1<=Speed_Right_Wheel_1] & 1<=Weight_Left_Wheel_off] | TheAltitude_1<=TheAltitude_19]] | TheAltitude_12<=0] | ~ [[[~ [[[1<=Speed_Right_Wheel_8 & [[TheAltitude_17<=SpeedPossibleVal_4 & AltitudePossibleVal_14<=0] | [1<=Weight_Left_Wheel_off | Speed_Right_Wheel_7<=0]]] & [[[AltitudePossibleVal_9<=AltitudePossibleVal_6 & Speed_Left_Wheel_5<=0] & [TheAltitude_18<=0 | TheAltitude_2<=0]] | [AltitudePossibleVal_18<=0 | [1<=AltitudePossibleVal_15 & AltitudePossibleVal_5<=Plane_On_Ground_Signal_no_T]]]]] & [[SpeedPossibleVal_7<=0 & [~ [1<=Weight_Left_Wheel_on] | [AltitudePossibleVal_16<=SpeedPossibleVal_4 & ~ [P2<=SpeedPossibleVal_3]]]] & [SpeedPossibleVal_5<=TheAltitude_17 | ~ [TheAltitude_18<=1]]]] & [~ [AltitudePossibleVal_5<=0] & 1<=SpeedPossibleVal_2]]]]]
normalized: ~ [E [true U ~ [[~ [[[~ [AltitudePossibleVal_5<=0] & 1<=SpeedPossibleVal_2] & [[[~ [TheAltitude_18<=1] | SpeedPossibleVal_5<=TheAltitude_17] & [[[~ [P2<=SpeedPossibleVal_3] & AltitudePossibleVal_16<=SpeedPossibleVal_4] | ~ [1<=Weight_Left_Wheel_on]] & SpeedPossibleVal_7<=0]] & ~ [[[[[1<=AltitudePossibleVal_15 & AltitudePossibleVal_5<=Plane_On_Ground_Signal_no_T] | AltitudePossibleVal_18<=0] | [[TheAltitude_18<=0 | TheAltitude_2<=0] & [AltitudePossibleVal_9<=AltitudePossibleVal_6 & Speed_Left_Wheel_5<=0]]] & [[[1<=Weight_Left_Wheel_off | Speed_Right_Wheel_7<=0] | [TheAltitude_17<=SpeedPossibleVal_4 & AltitudePossibleVal_14<=0]] & 1<=Speed_Right_Wheel_8]]]]]] | [[[[[~ [[Weight_Left_Wheel_on<=0 & 1<=TheAltitude_2]] | 1<=Speed_Right_Wheel_1] & 1<=Weight_Left_Wheel_off] | TheAltitude_1<=TheAltitude_19] | ~ [WeightPossibleVal_off<=AltitudePossibleVal_1]] | TheAltitude_12<=0]]]]]

abstracting: (TheAltitude_12<=0)
states: 41,406 (4)
abstracting: (WeightPossibleVal_off<=AltitudePossibleVal_1)
states: 43,463 (4)
abstracting: (TheAltitude_1<=TheAltitude_19)
states: 41,406 (4)
abstracting: (1<=Weight_Left_Wheel_off)
states: 7,623 (3)
abstracting: (1<=Speed_Right_Wheel_1)
states: 3,951 (3)
abstracting: (1<=TheAltitude_2)
states: 2,057 (3)
abstracting: (Weight_Left_Wheel_on<=0)
states: 35,840 (4)
abstracting: (1<=Speed_Right_Wheel_8)
states: 3,951 (3)
abstracting: (AltitudePossibleVal_14<=0)
states: 0
abstracting: (TheAltitude_17<=SpeedPossibleVal_4)
states: 43,463 (4)
abstracting: (Speed_Right_Wheel_7<=0)
states: 39,512 (4)
abstracting: (1<=Weight_Left_Wheel_off)
states: 7,623 (3)
abstracting: (Speed_Left_Wheel_5<=0)
states: 39,514 (4)
abstracting: (AltitudePossibleVal_9<=AltitudePossibleVal_6)
states: 43,463 (4)
abstracting: (TheAltitude_2<=0)
states: 41,406 (4)
abstracting: (TheAltitude_18<=0)
states: 41,406 (4)
abstracting: (AltitudePossibleVal_18<=0)
states: 0
abstracting: (AltitudePossibleVal_5<=Plane_On_Ground_Signal_no_T)
states: 10,297 (4)
abstracting: (1<=AltitudePossibleVal_15)
states: 43,463 (4)
abstracting: (SpeedPossibleVal_7<=0)
states: 0
abstracting: (1<=Weight_Left_Wheel_on)
states: 7,623 (3)
abstracting: (AltitudePossibleVal_16<=SpeedPossibleVal_4)
states: 43,463 (4)
abstracting: (P2<=SpeedPossibleVal_3)
states: 43,463 (4)
abstracting: (SpeedPossibleVal_5<=TheAltitude_17)
states: 2,057 (3)
abstracting: (TheAltitude_18<=1)
states: 43,463 (4)
abstracting: (1<=SpeedPossibleVal_2)
states: 43,463 (4)
abstracting: (AltitudePossibleVal_5<=0)
states: 0
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-12 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.012sec

checking: EF [[[~ [[1<=SpeedPossibleVal_4 | Weight_Left_Wheel_on<=0]] & [~ [[[[Plane_On_Ground_Signal_no_T<=Speed_Right_Wheel_1 & Speed_Left_Wheel_4<=0] & [~ [WeightPossibleVal_off<=Speed_Left_Wheel_10] & [[TheAltitude_1<=0 | TheAltitude_9<=0] | Weight_Left_Wheel_off<=Weight_Left_Wheel_on]]] | ~ [TheAltitude_16<=Speed_Left_Wheel_6]]] | [1<=SpeedPossibleVal_10 & [1<=TheAltitude_20 | [~ [[~ [P1<=0] & [1<=Speed_Left_Wheel_3 & 1<=AltitudePossibleVal_20]]] | ~ [[SpeedPossibleVal_3<=Speed_Left_Wheel_3 & P6<=1]]]]]]] | ~ [[~ [[[[~ [1<=AltitudePossibleVal_8] & SpeedPossibleVal_9<=Speed_Right_Wheel_2] & 1<=AltitudePossibleVal_1] | [[~ [[AltitudePossibleVal_8<=AltitudePossibleVal_17 | 1<=Speed_Right_Wheel_1]] & P1<=Speed_Right_Wheel_3] | ~ [[[1<=AltitudePossibleVal_16 & AltitudePossibleVal_5<=0] | ~ [AltitudePossibleVal_14<=0]]]]]] | [[~ [[[1<=WeightPossibleVal_on | 1<=AltitudePossibleVal_8] | Speed_Left_Wheel_7<=TheAltitude_16]] & [1<=Plane_On_Ground_Signal_no_F | 1<=AltitudePossibleVal_12]] | [[[~ [[1<=Speed_Left_Wheel_3 & AltitudePossibleVal_14<=Weight_Left_Wheel_off]] & [~ [AltitudePossibleVal_2<=Speed_Right_Wheel_10] | [AltitudePossibleVal_7<=0 | stp5<=0]]] | ~ [[[Speed_Right_Wheel_1<=0 & Weight_Left_Wheel_off<=1] & [1<=AltitudePossibleVal_8 | 1<=AltitudePossibleVal_13]]]] | [~ [[[1<=Speed_Right_Wheel_8 | 1<=TheAltitude_5] & Speed_Left_Wheel_10<=SpeedPossibleVal_10]] | 1<=AltitudePossibleVal_2]]]]]]]
normalized: E [true U [~ [[[[[1<=AltitudePossibleVal_2 | ~ [[Speed_Left_Wheel_10<=SpeedPossibleVal_10 & [1<=Speed_Right_Wheel_8 | 1<=TheAltitude_5]]]] | [~ [[[1<=AltitudePossibleVal_8 | 1<=AltitudePossibleVal_13] & [Speed_Right_Wheel_1<=0 & Weight_Left_Wheel_off<=1]]] | [[[AltitudePossibleVal_7<=0 | stp5<=0] | ~ [AltitudePossibleVal_2<=Speed_Right_Wheel_10]] & ~ [[1<=Speed_Left_Wheel_3 & AltitudePossibleVal_14<=Weight_Left_Wheel_off]]]]] | [[1<=Plane_On_Ground_Signal_no_F | 1<=AltitudePossibleVal_12] & ~ [[Speed_Left_Wheel_7<=TheAltitude_16 | [1<=WeightPossibleVal_on | 1<=AltitudePossibleVal_8]]]]] | ~ [[[~ [[~ [AltitudePossibleVal_14<=0] | [1<=AltitudePossibleVal_16 & AltitudePossibleVal_5<=0]]] | [P1<=Speed_Right_Wheel_3 & ~ [[AltitudePossibleVal_8<=AltitudePossibleVal_17 | 1<=Speed_Right_Wheel_1]]]] | [1<=AltitudePossibleVal_1 & [SpeedPossibleVal_9<=Speed_Right_Wheel_2 & ~ [1<=AltitudePossibleVal_8]]]]]]] | [[[1<=SpeedPossibleVal_10 & [1<=TheAltitude_20 | [~ [[SpeedPossibleVal_3<=Speed_Left_Wheel_3 & P6<=1]] | ~ [[[1<=Speed_Left_Wheel_3 & 1<=AltitudePossibleVal_20] & ~ [P1<=0]]]]]] | ~ [[~ [TheAltitude_16<=Speed_Left_Wheel_6] | [[[Weight_Left_Wheel_off<=Weight_Left_Wheel_on | [TheAltitude_1<=0 | TheAltitude_9<=0]] & ~ [WeightPossibleVal_off<=Speed_Left_Wheel_10]] & [Plane_On_Ground_Signal_no_T<=Speed_Right_Wheel_1 & Speed_Left_Wheel_4<=0]]]]] & ~ [[1<=SpeedPossibleVal_4 | Weight_Left_Wheel_on<=0]]]]]

abstracting: (Weight_Left_Wheel_on<=0)
states: 35,840 (4)
abstracting: (1<=SpeedPossibleVal_4)
states: 43,463 (4)
abstracting: (Speed_Left_Wheel_4<=0)
states: 39,514 (4)
abstracting: (Plane_On_Ground_Signal_no_T<=Speed_Right_Wheel_1)
states: 34,102 (4)
abstracting: (WeightPossibleVal_off<=Speed_Left_Wheel_10)
states: 3,949 (3)
abstracting: (TheAltitude_9<=0)
states: 41,406 (4)
abstracting: (TheAltitude_1<=0)
states: 41,406 (4)
abstracting: (Weight_Left_Wheel_off<=Weight_Left_Wheel_on)
states: 35,840 (4)
abstracting: (TheAltitude_16<=Speed_Left_Wheel_6)
states: 41,593 (4)
abstracting: (P1<=0)
states: 20,594 (4)
abstracting: (1<=AltitudePossibleVal_20)
states: 43,463 (4)
abstracting: (1<=Speed_Left_Wheel_3)
states: 3,949 (3)
abstracting: (P6<=1)
states: 43,463 (4)
abstracting: (SpeedPossibleVal_3<=Speed_Left_Wheel_3)
states: 3,949 (3)
abstracting: (1<=TheAltitude_20)
states: 2,057 (3)
abstracting: (1<=SpeedPossibleVal_10)
states: 43,463 (4)
abstracting: (1<=AltitudePossibleVal_8)
states: 43,463 (4)
abstracting: (SpeedPossibleVal_9<=Speed_Right_Wheel_2)
states: 3,951 (3)
abstracting: (1<=AltitudePossibleVal_1)
states: 43,463 (4)
abstracting: (1<=Speed_Right_Wheel_1)
states: 3,951 (3)
abstracting: (AltitudePossibleVal_8<=AltitudePossibleVal_17)
states: 43,463 (4)
abstracting: (P1<=Speed_Right_Wheel_3)
states: 22,673 (4)
abstracting: (AltitudePossibleVal_5<=0)
states: 0
abstracting: (1<=AltitudePossibleVal_16)
states: 43,463 (4)
abstracting: (AltitudePossibleVal_14<=0)
states: 0
abstracting: (1<=AltitudePossibleVal_8)
states: 43,463 (4)
abstracting: (1<=WeightPossibleVal_on)
states: 43,463 (4)
abstracting: (Speed_Left_Wheel_7<=TheAltitude_16)
states: 39,701 (4)
abstracting: (1<=AltitudePossibleVal_12)
states: 43,463 (4)
abstracting: (1<=Plane_On_Ground_Signal_no_F)
states: 1
abstracting: (AltitudePossibleVal_14<=Weight_Left_Wheel_off)
states: 7,623 (3)
abstracting: (1<=Speed_Left_Wheel_3)
states: 3,949 (3)
abstracting: (AltitudePossibleVal_2<=Speed_Right_Wheel_10)
states: 3,951 (3)
abstracting: (stp5<=0)
states: 39,512 (4)
abstracting: (AltitudePossibleVal_7<=0)
states: 0
abstracting: (Weight_Left_Wheel_off<=1)
states: 43,463 (4)
abstracting: (Speed_Right_Wheel_1<=0)
states: 39,512 (4)
abstracting: (1<=AltitudePossibleVal_13)
states: 43,463 (4)
abstracting: (1<=AltitudePossibleVal_8)
states: 43,463 (4)
abstracting: (1<=TheAltitude_5)
states: 2,057 (3)
abstracting: (1<=Speed_Right_Wheel_8)
states: 3,951 (3)
abstracting: (Speed_Left_Wheel_10<=SpeedPossibleVal_10)
states: 43,463 (4)
abstracting: (1<=AltitudePossibleVal_2)
states: 43,463 (4)
-> the formula is FALSE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-08 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.020sec

checking: AG [~ [[[[[~ [[[68<=stp4 | stp5<=69] | [[sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp5 & 20<=P4] & sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P1]]] & ~ [P5<=70]] & [sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=80 | [P2<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1) & [39<=stp2 | [[P4<=stp3 | P2<=P1] | [sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=64 & sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=71]]]]]] | ~ [stp1<=32]] & P5<=43]]]
normalized: ~ [E [true U [P5<=43 & [~ [stp1<=32] | [[sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=80 | [P2<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1) & [39<=stp2 | [[sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=64 & sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=71] | [P4<=stp3 | P2<=P1]]]]] & [~ [P5<=70] & ~ [[[sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P1 & [sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp5 & 20<=P4]] | [68<=stp4 | stp5<=69]]]]]]]]]

abstracting: (stp5<=69)
states: 43,463 (4)
abstracting: (68<=stp4)
states: 0
abstracting: (20<=P4)
states: 0
abstracting: (sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp5)
states: 0
abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P1)
states: 0
abstracting: (P5<=70)
states: 43,463 (4)
abstracting: (P2<=P1)
states: 35,840 (4)
abstracting: (P4<=stp3)
states: 43,342 (4)
abstracting: (sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=71)
states: 43,463 (4)
abstracting: (sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=64)
states: 43,463 (4)
abstracting: (39<=stp2)
states: 0
abstracting: (P2<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1))
states: 42,770 (4)
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=80)
states: 43,463 (4)
abstracting: (stp1<=32)
states: 43,463 (4)
abstracting: (P5<=43)
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-03 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 4.708sec

checking: AG [[~ [99<=P3] | [~ [15<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)] & [~ [[~ [[stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1) | 14<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)]] & [[[[sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=30 | stp3<=P6] | ~ [40<=sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)]] | [[sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=P6 | P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)] & 69<=sum(WeightPossibleVal_off, WeightPossibleVal_on)]] | [43<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on) | ~ [sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=46]]]]] & 63<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]]]]
normalized: ~ [E [true U ~ [[[~ [15<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)] & [63<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1) & ~ [[~ [[stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1) | 14<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)]] & [[[[sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=30 | stp3<=P6] | ~ [40<=sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)]] | [69<=sum(WeightPossibleVal_off, WeightPossibleVal_on) & [sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=P6 | P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)]]] | [43<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on) | ~ [sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=46]]]]]]] | ~ [99<=P3]]]]]

abstracting: (99<=P3)
states: 0
abstracting: (sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=46)
states: 43,463 (4)
abstracting: (43<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on))
states: 0
abstracting: (P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 43,463 (4)
abstracting: (sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=P6)
states: 13,323 (4)
abstracting: (69<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 0
abstracting: (40<=sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1))
states: 0
abstracting: (stp3<=P6)
states: 41,890 (4)
abstracting: (sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)<=30)
states: 43,463 (4)
abstracting: (14<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1))
states: 0
abstracting: (stp2<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 42,308 (4)
abstracting: (63<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1))
states: 0
abstracting: (15<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 0
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-01 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 2.484sec

checking: AG [~ [[~ [[~ [[~ [[sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)<=stp4 | stp4<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]] & [~ [stp4<=16] & ~ [sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=96]]]] & ~ [[stp2<=P3 | [68<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1) | 67<=stp5]]]]] & [[37<=P6 & sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)] & ~ [[[~ [[stp5<=73 & stp4<=49]] & [[stp5<=86 & P3<=39] & 31<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1)]] | [[[P3<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1) | 95<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)] | [sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=stp1 & P4<=stp1]] | [[sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=95 | 77<=stp3] | ~ [sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=P1]]]]]]]]]
normalized: ~ [E [true U [[[37<=P6 & sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)] & ~ [[[[[sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=stp1 & P4<=stp1] | [P3<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1) | 95<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)]] | [~ [sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=P1] | [sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=95 | 77<=stp3]]] | [[31<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1) & [stp5<=86 & P3<=39]] & ~ [[stp5<=73 & stp4<=49]]]]]] & ~ [[~ [[stp2<=P3 | [68<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1) | 67<=stp5]]] & ~ [[[~ [stp4<=16] & ~ [sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=96]] & ~ [[sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)<=stp4 | stp4<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]]]]]]]]]

abstracting: (stp4<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1))
states: 43,463 (4)
abstracting: (sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)<=stp4)
states: 6,063 (3)
abstracting: (sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1)<=96)
states: 43,463 (4)
abstracting: (stp4<=16)
states: 43,463 (4)
abstracting: (67<=stp5)
states: 0
abstracting: (68<=sum(Speed_Right_Wheel_10, Speed_Right_Wheel_9, Speed_Right_Wheel_8, Speed_Right_Wheel_7, Speed_Right_Wheel_6, Speed_Right_Wheel_5, Speed_Right_Wheel_4, Speed_Right_Wheel_3, Speed_Right_Wheel_2, Speed_Right_Wheel_1))
states: 0
abstracting: (stp2<=P3)
states: 30,758 (4)
abstracting: (stp4<=49)
states: 43,463 (4)
abstracting: (stp5<=73)
states: 43,463 (4)
abstracting: (P3<=39)
states: 43,463 (4)
abstracting: (stp5<=86)
states: 43,463 (4)
abstracting: (31<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1))
states: 0
abstracting: (77<=stp3)
states: 0
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=95)
states: 43,463 (4)
abstracting: (sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=P1)
states: 0
abstracting: (95<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1))
states: 0
abstracting: (P3<=sum(Speed_Left_Wheel_10, Speed_Left_Wheel_9, Speed_Left_Wheel_8, Speed_Left_Wheel_7, Speed_Left_Wheel_6, Speed_Left_Wheel_5, Speed_Left_Wheel_4, Speed_Left_Wheel_3, Speed_Left_Wheel_2, Speed_Left_Wheel_1))
states: 43,232 (4)
abstracting: (P4<=stp1)
states: 43,342 (4)
abstracting: (sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1)<=stp1)
states: 0
abstracting: (sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)<=sum(AltitudePossibleVal_20, AltitudePossibleVal_19, AltitudePossibleVal_18, AltitudePossibleVal_17, AltitudePossibleVal_16, AltitudePossibleVal_15, AltitudePossibleVal_14, AltitudePossibleVal_13, AltitudePossibleVal_12, AltitudePossibleVal_11, AltitudePossibleVal_10, AltitudePossibleVal_9, AltitudePossibleVal_8, AltitudePossibleVal_7, AltitudePossibleVal_6, AltitudePossibleVal_5, AltitudePossibleVal_4, AltitudePossibleVal_3, AltitudePossibleVal_2, AltitudePossibleVal_1))
states: 43,463 (4)
abstracting: (37<=P6)
states: 0
-> the formula is TRUE

FORMULA AirplaneLD-PT-0010-ReachabilityCardinality-06 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 5.167sec

totally nodes used: 23299 (2.3e+04)
number of garbage collections: 0
fire ops cache: hits/miss/sum: 40864 115501 156365
used/not used/entry size/cache size: 116411 66992453 16 1024MB
basic ops cache: hits/miss/sum: 58122 138207 196329
used/not used/entry size/cache size: 179403 16597813 12 192MB
unary ops cache: hits/miss/sum: 0 0 0
used/not used/entry size/cache size: 0 16777216 8 128MB
abstract ops cache: hits/miss/sum: 0 14701577 14701577
used/not used/entry size/cache size: 1 16777215 12 192MB
state nr cache: hits/miss/sum: 5878 11689 17567
used/not used/entry size/cache size: 11689 8376919 32 256MB
max state cache: hits/miss/sum: 0 0 0
used/not used/entry size/cache size: 0 8388608 32 256MB
uniqueHash elements/entry size/size: 67108864 4 256MB
0 67085784
1 22872
2 201
3 4
4 2
5 1
6 0
7 0
8 0
9 0
>= 10 0

Total processing time: 0m17.211sec


BK_STOP 1678388071162

--------------------
content from stderr:

check for maximal unmarked siphon
ok
check for constant places
SpeedPossibleVal_1
SpeedPossibleVal_2
SpeedPossibleVal_3
SpeedPossibleVal_4
SpeedPossibleVal_5
SpeedPossibleVal_6
SpeedPossibleVal_7
SpeedPossibleVal_8
SpeedPossibleVal_9
SpeedPossibleVal_10
AltitudePossibleVal_1
AltitudePossibleVal_2
AltitudePossibleVal_3
AltitudePossibleVal_4
AltitudePossibleVal_5
AltitudePossibleVal_6
AltitudePossibleVal_7
AltitudePossibleVal_8
AltitudePossibleVal_9
AltitudePossibleVal_10
AltitudePossibleVal_11
AltitudePossibleVal_12
AltitudePossibleVal_13
AltitudePossibleVal_14
AltitudePossibleVal_15
AltitudePossibleVal_16
AltitudePossibleVal_17
AltitudePossibleVal_18
AltitudePossibleVal_19
AltitudePossibleVal_20
WeightPossibleVal_on
WeightPossibleVal_off
found 32 constant places
check if there are places and transitions
ok
check if there are transitions without pre-places
ok
check if at least one transition is enabled in m0
ok
check if there are transitions that can never fire
ok


initing FirstDep: 0m 0.000sec


iterations count:1219 (13), effective:54 (0)

initing FirstDep: 0m 0.000sec


iterations count:170 (1), effective:5 (0)

Sequence of Actions to be Executed by the VM

This is useful if one wants to reexecute the tool in the VM from the submitted image disk.

set -x
# this is for BenchKit: configuration of major elements for the test
export BK_INPUT="AirplaneLD-PT-0010"
export BK_EXAMINATION="ReachabilityCardinality"
export BK_TOOL="marcie"
export BK_RESULT_DIR="/tmp/BK_RESULTS/OUTPUTS"
export BK_TIME_CONFINEMENT="3600"
export BK_MEMORY_CONFINEMENT="16384"
export BK_BIN_PATH="/home/mcc/BenchKit/bin/"

# this is specific to your benchmark or test

export BIN_DIR="$HOME/BenchKit/bin"

# remove the execution directoty if it exists (to avoid increse of .vmdk images)
if [ -d execution ] ; then
rm -rf execution
fi

# this is for BenchKit: explicit launching of the test
echo "====================================================================="
echo " Generated by BenchKit 2-5348"
echo " Executing tool marcie"
echo " Input is AirplaneLD-PT-0010, examination is ReachabilityCardinality"
echo " Time confinement is $BK_TIME_CONFINEMENT seconds"
echo " Memory confinement is 16384 MBytes"
echo " Number of cores is 1"
echo " Run identifier is r001-oct2-167813588400246"
echo "====================================================================="
echo
echo "--------------------"
echo "preparation of the directory to be used:"

tar xzf /home/mcc/BenchKit/INPUTS/AirplaneLD-PT-0010.tgz
mv AirplaneLD-PT-0010 execution
cd execution
if [ "ReachabilityCardinality" = "ReachabilityDeadlock" ] || [ "ReachabilityCardinality" = "UpperBounds" ] || [ "ReachabilityCardinality" = "QuasiLiveness" ] || [ "ReachabilityCardinality" = "StableMarking" ] || [ "ReachabilityCardinality" = "Liveness" ] || [ "ReachabilityCardinality" = "OneSafe" ] || [ "ReachabilityCardinality" = "StateSpace" ]; then
rm -f GenericPropertiesVerdict.xml
fi
pwd
ls -lh

echo
echo "--------------------"
echo "content from stdout:"
echo
echo "=== Data for post analysis generated by BenchKit (invocation template)"
echo
if [ "ReachabilityCardinality" = "UpperBounds" ] ; then
echo "The expected result is a vector of positive values"
echo NUM_VECTOR
elif [ "ReachabilityCardinality" != "StateSpace" ] ; then
echo "The expected result is a vector of booleans"
echo BOOL_VECTOR
else
echo "no data necessary for post analysis"
fi
echo
if [ -f "ReachabilityCardinality.txt" ] ; then
echo "here is the order used to build the result vector(from text file)"
for x in $(grep Property ReachabilityCardinality.txt | cut -d ' ' -f 2 | sort -u) ; do
echo "FORMULA_NAME $x"
done
elif [ -f "ReachabilityCardinality.xml" ] ; then # for cunf (txt files deleted;-)
echo echo "here is the order used to build the result vector(from xml file)"
for x in $(grep '' ReachabilityCardinality.xml | cut -d '>' -f 2 | cut -d '<' -f 1 | sort -u) ; do
echo "FORMULA_NAME $x"
done
elif [ "ReachabilityCardinality" = "ReachabilityDeadlock" ] || [ "ReachabilityCardinality" = "QuasiLiveness" ] || [ "ReachabilityCardinality" = "StableMarking" ] || [ "ReachabilityCardinality" = "Liveness" ] || [ "ReachabilityCardinality" = "OneSafe" ] ; then
echo "FORMULA_NAME ReachabilityCardinality"
fi
echo
echo "=== Now, execution of the tool begins"
echo
echo -n "BK_START "
date -u +%s%3N
echo
timeout -s 9 $BK_TIME_CONFINEMENT bash -c "/home/mcc/BenchKit/BenchKit_head.sh 2> STDERR ; echo ; echo -n \"BK_STOP \" ; date -u +%s%3N"
if [ $? -eq 137 ] ; then
echo
echo "BK_TIME_CONFINEMENT_REACHED"
fi
echo
echo "--------------------"
echo "content from stderr:"
echo
cat STDERR ;