Execution Chart

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

Trace from the execution

Waiting for the VM to be ready (probing ssh)
........
=====================================================================
Generated by BenchKit 2-2979
Executing tool marcie
Input is AirplaneLD-PT-0010, examination is CTLCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r209su-blw3-146445824500084
=====================================================================

--------------------
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-COL-0010-CTLCardinality-0
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-1
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-10
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-11
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-12
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-13
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-14
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-15
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-2
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-3
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-4
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-5
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-6
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-7
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-8
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-9

=== Now, execution of the tool begins

BK_START 1464677918337


Marcie rev. 8535M (built: crohr on 2016-04-27)
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: marcie --net-file=model.pnml --mcc-file=CTLCardinality.xml --mcc-mode --memory=6 --suppress

parse successfull
net created successfully

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

net check time: 0m 0.000sec

parse formulas
formulas created successfully
place and transition orderings generation:0m 0.000sec

init dd package: 0m 4.292sec


RS generation: 0m 0.034sec


-> reachability set: #nodes 353 (3.5e+02) #states 43,463 (4)



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

checking: ~ [~ [AG [P3<=stp1]]]
normalized: ~ [E [true U ~ [P3<=stp1]]]

abstracting: (P3<=stp1) states: 40,922 (4)
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-4 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.011sec

checking: AG [1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)]
normalized: ~ [E [true U ~ [1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)]]]

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

FORMULA AirplaneLD-COL-0010-CTLCardinality-14 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.043sec

checking: ~ [AG [AX [P4<=stp5]]]
normalized: E [true U EX [~ [P4<=stp5]]]

abstracting: (P4<=stp5) states: 43,353 (4)
.-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-15 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.056sec

checking: AF [sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P3]
normalized: ~ [EG [~ [sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P3]]]

abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P3) states: 0

EG iterations: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-2 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.045sec

checking: [EF [~ [[1<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on) & 2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)]]] & EG [[P6<=P2 | 2<=P1]]]
normalized: [EG [[P6<=P2 | 2<=P1]] & E [true U ~ [[1<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on) & 2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)]]]]

abstracting: (2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)) states: 0
abstracting: (1<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)) states: 15,246 (4)
abstracting: (2<=P1) states: 0
abstracting: (P6<=P2) states: 33,165 (4)
...........
EG iterations: 11
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-1 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.162sec

checking: EG [~ [1<=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: EG [~ [1<=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: (1<=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: 39,510 (4)
..........
EG iterations: 10
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-10 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.070sec

checking: EX [EG [[P6<=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) | 1<=stp3]]]
normalized: EX [EG [[P6<=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) | 1<=stp3]]]

abstracting: (1<=stp3) states: 2,057 (3)
abstracting: (P6<=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: 42,525 (4)
.......
EG iterations: 7
.-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-11 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.097sec

checking: AG [[EX [stp2<=P4] | ~ [[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) | 3<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)]]]]
normalized: ~ [E [true U ~ [[~ [[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) | 3<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)]] | EX [stp2<=P4]]]]]

abstracting: (stp2<=P4) states: 30,758 (4)
.abstracting: (3<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)) states: 0
abstracting: (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)) states: 39,490 (4)
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-7 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.141sec

checking: AF [~ [EF [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)<=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: ~ [EG [E [true U 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)<=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: (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)<=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: 43,463 (4)

EG iterations: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-0 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.042sec

checking: EF [~ [AF [stp2<=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)]]]
normalized: E [true U EG [~ [stp2<=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)]]]

abstracting: (stp2<=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: 42,858 (4)
......
EG iterations: 6
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-8 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 1.229sec

checking: ~ [[AG [~ [sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp5]] & A [1<=stp2 U 1<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]]]
normalized: ~ [[[~ [EG [~ [1<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]]] & ~ [E [~ [1<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)] U [~ [1<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)] & ~ [1<=stp2]]]]] & ~ [E [true U sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp5]]]]

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: (1<=stp2) states: 12,705 (4)
abstracting: (1<=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: (1<=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: (1<=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)
.
EG iterations: 1
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-3 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.164sec

checking: EG [[EX [P2<=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)] & EF [sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=P6]]]
normalized: EG [[E [true U sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=P6] & EX [P2<=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)]]]

abstracting: (P2<=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: (sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=P6) states: 28,217 (4)
...........
EG iterations: 11
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-12 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 1.033sec

checking: [~ [[AG [sum(Weight_Left_Wheel_off, Weight_Left_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(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]]] & [~ [1<=stp3] | P3<=stp3]]
normalized: [[P3<=stp3 | ~ [1<=stp3]] & ~ [[~ [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] | ~ [E [true U ~ [sum(Weight_Left_Wheel_off, Weight_Left_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)]]]]]]

abstracting: (sum(Weight_Left_Wheel_off, Weight_Left_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: (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: (1<=stp3) states: 2,057 (3)
abstracting: (P3<=stp3) states: 41,043 (4)
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-13 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 2.283sec

checking: [[~ [~ [~ [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)]]] | [[~ [3<=stp1] | [2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | P2<=P4]] & AF [2<=stp3]]] & ~ [1<=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)]]
normalized: [~ [1<=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)] & [~ [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)] | [[~ [3<=stp1] | [2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | P2<=P4]] & ~ [EG [~ [2<=stp3]]]]]]

abstracting: (2<=stp3) states: 0

EG iterations: 0
abstracting: (P2<=P4) states: 35,840 (4)
abstracting: (2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)) states: 0
abstracting: (3<=stp1) states: 0
abstracting: (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)) states: 43,463 (4)
abstracting: (1<=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: 41,140 (4)
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-6 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 1.271sec

checking: [EF [[[P4<=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) & 3<=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)] & [P2<=P3 | stp2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)]]] & AG [[[P3<=P6 & P6<=stp4] | ~ [3<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)]]]]
normalized: [~ [E [true U ~ [[~ [3<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)] | [P3<=P6 & P6<=stp4]]]]] & E [true U [[P2<=P3 | stp2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)] & [P4<=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) & 3<=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)]]]]

abstracting: (3<=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: (P4<=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: 43,342 (4)
abstracting: (stp2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)) states: 33,299 (4)
abstracting: (P2<=P3) states: 35,840 (4)
abstracting: (P6<=stp4) states: 34,100 (4)
abstracting: (P3<=P6) states: 40,922 (4)
abstracting: (3<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)) states: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-CTLCardinality-9 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 1.933sec

checking: E [[[sum(WeightPossibleVal_off, WeightPossibleVal_on)<=stp3 & 3<=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(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)<=stp2]] U EG [2<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]]
normalized: E [[~ [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)<=stp2] | [sum(WeightPossibleVal_off, WeightPossibleVal_on)<=stp3 & 3<=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)]] U EG [2<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]]

abstracting: (2<=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)

EG iterations: 0
abstracting: (3<=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: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=stp3) states: 0
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)<=stp2) states: 14,423 (4)
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-CTLCardinality-5 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 1.730sec


Total processing time: 0m16.342sec


BK_STOP 1464677934712

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

check for maximal unmarked siphon
ok
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

353
iterations count:1124 (12), effective:54 (0)

initing FirstDep: 0m 0.000sec


iterations count:99 (1), effective:4 (0)

iterations count:309 (3), effective:60 (0)

iterations count:88 (1), effective:0 (0)

iterations count:564 (6), effective:37 (0)

iterations count:88 (1), effective:0 (0)

iterations count:120 (1), effective:2 (0)

iterations count:88 (1), effective:0 (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="CTLCardinality"
export BK_TOOL="marcie"
export BK_RESULT_DIR="/home/hulinhub/BK_RESULTS/OUTPUTS"
export BK_TIME_CONFINEMENT="3600"
export BK_MEMORY_CONFINEMENT="16384"

# 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

tar xzf /home/mcc/BenchKit/INPUTS/AirplaneLD-PT-0010.tgz
mv AirplaneLD-PT-0010 execution

# this is for BenchKit: explicit launching of the test

cd execution
echo "====================================================================="
echo " Generated by BenchKit 2-2979"
echo " Executing tool marcie"
echo " Input is AirplaneLD-PT-0010, examination is CTLCardinality"
echo " Time confinement is $BK_TIME_CONFINEMENT seconds"
echo " Memory confinement is 16384 MBytes"
echo " Number of cores is 1"
echo " Run identifier is r209su-blw3-146445824500084"
echo "====================================================================="
echo
echo "--------------------"
echo "content from stdout:"
echo
echo "=== Data for post analysis generated by BenchKit (invocation template)"
echo
if [ "CTLCardinality" = "UpperBounds" ] ; then
echo "The expected result is a vector of positive values"
echo NUM_VECTOR
elif [ "CTLCardinality" != "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 "CTLCardinality.txt" ] ; then
echo "here is the order used to build the result vector(from text file)"
for x in $(grep Property CTLCardinality.txt | cut -d ' ' -f 2 | sort -u) ; do
echo "FORMULA_NAME $x"
done
elif [ -f "CTLCardinality.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 '' CTLCardinality.xml | cut -d '>' -f 2 | cut -d '<' -f 1 | sort -u) ; do
echo "FORMULA_NAME $x"
done
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 ;