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 2-3254
Executing tool marcie
Input is S_AirplaneLD-PT-0010, examination is ReachabilityCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r081-csrt-149441064000061
=====================================================================

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

=== Now, execution of the tool begins

BK_START 1494883769887

timeout --kill-after=10s --signal=SIGINT 1m for testing only

Marcie rev. 8852M (built: crohr on 2017-05-03)
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=ReachabilityCardinality.xml --memory=6

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 1.254sec


RS generation: 0m 0.004sec


-> reachability set: #nodes 261 (2.6e+02) #states 43,463 (4)



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

checking: EF [~ [~ [3<=stp5]]]
normalized: E [true U 3<=stp5]

abstracting: (3<=stp5)
states: 0
-> the formula is FALSE

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

MC time: 0m 0.000sec

checking: EF [3<=stp2]
normalized: E [true U 3<=stp2]

abstracting: (3<=stp2)
states: 0
-> the formula is FALSE

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

MC time: 0m 0.000sec

checking: EF [2<=stp4]
normalized: E [true U 2<=stp4]

abstracting: (2<=stp4)
states: 0
-> the formula is FALSE

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

MC time: 0m 0.000sec

checking: EF [2<=stp2]
normalized: E [true U 2<=stp2]

abstracting: (2<=stp2)
states: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-ReachabilityCardinality-14 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.000sec

checking: EF [~ [~ [[1<=stp1 & 2<=stp3]]]]
normalized: E [true U [1<=stp1 & 2<=stp3]]

abstracting: (2<=stp3)
states: 0
abstracting: (1<=stp1)
states: 7,623 (3)
-> the formula is FALSE

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

MC time: 0m 0.000sec

checking: AG [[2<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | ~ [~ [1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)]]]]
normalized: ~ [E [true U ~ [[2<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | 1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)]]]]

abstracting: (1<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 43,463 (4)
abstracting: (2<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-ReachabilityCardinality-6 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.038sec

checking: EF [[[2<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) & ~ [P6<=stp5]] & [[1<=P3 | 1<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)] | [1<=stp5 & 3<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)]]]]
normalized: E [true U [[[1<=P3 | 1<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)] | [1<=stp5 & 3<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)]] & [~ [P6<=stp5] & 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: (P6<=stp5)
states: 34,101 (4)
abstracting: (3<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on))
states: 0
abstracting: (1<=stp5)
states: 3,951 (3)
abstracting: (1<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
states: 10,298 (4)
abstracting: (1<=P3)
states: 2,541 (3)
-> the formula is FALSE

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

MC time: 0m 0.061sec

checking: EF [~ [1<=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 ~ [1<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]]

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)
-> the formula is FALSE

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

MC time: 0m 0.019sec

checking: EF [[1<=P3 | [[sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P1 | 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)<=P4] & [3<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | 3<=P2]]]]
normalized: E [true U [[[sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P1 | 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)<=P4] & [3<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | 3<=P2]] | 1<=P3]]

abstracting: (1<=P3)
states: 2,541 (3)
abstracting: (3<=P2)
states: 0
abstracting: (3<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T))
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)<=P4)
states: 4,083 (3)
abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P1)
states: 0
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-ReachabilityCardinality-0 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.060sec

checking: EF [[[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) & [sum(WeightPossibleVal_off, WeightPossibleVal_on)<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on) | 2<=stp1]] & ~ [[2<=P4 & 3<=stp2]]]]
normalized: E [true U [~ [[2<=P4 & 3<=stp2]] & [[sum(WeightPossibleVal_off, WeightPossibleVal_on)<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on) | 2<=stp1] & 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)]]]

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)
abstracting: (2<=stp1)
states: 0
abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on))
states: 0
abstracting: (3<=stp2)
states: 0
abstracting: (2<=P4)
states: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-ReachabilityCardinality-15 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.039sec

checking: EF [~ [[[P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | 2<=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)] | 2<=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 ~ [[[P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | 2<=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)] | 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)
abstracting: (2<=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: (P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 43,463 (4)
-> the formula is FALSE

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

MC time: 0m 0.058sec

checking: EF [[[~ [2<=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)] & ~ [2<=stp3]] & [sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=stp2 & 2<=P4]]]
normalized: E [true U [[~ [2<=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)] & ~ [2<=stp3]] & [sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=stp2 & 2<=P4]]]

abstracting: (2<=P4)
states: 0
abstracting: (sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)<=stp2)
states: 33,299 (4)
abstracting: (2<=stp3)
states: 0
abstracting: (2<=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)
-> the formula is FALSE

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

MC time: 0m 0.040sec

checking: EF [[[[1<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1) | P3<=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)] & ~ [2<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]] & [[P2<=stp2 & P1<=P5] & [2<=P1 & 2<=P1]]]]
normalized: E [true U [[[2<=P1 & 2<=P1] & [P2<=stp2 & P1<=P5]] & [~ [2<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)] & [1<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1) | P3<=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: (P3<=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: 43,232 (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: (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)
abstracting: (P1<=P5)
states: 20,594 (4)
abstracting: (P2<=stp2)
states: 38,381 (4)
abstracting: (2<=P1)
states: 0
abstracting: (2<=P1)
states: 0
-> the formula is FALSE

FORMULA AirplaneLD-COL-0010-ReachabilityCardinality-5 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.020sec

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)<=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)]
normalized: ~ [E [true U ~ [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(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(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(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)
-> the formula is TRUE

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

MC time: 0m 4.326sec

checking: EF [[P2<=P4 & [[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)<=P4 & 3<=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(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp1 | sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp3]]]]
normalized: E [true U [P2<=P4 & [[sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp1 | sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=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)<=P4 & 3<=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: (3<=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: (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)<=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)<=stp3)
states: 0
abstracting: (sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)<=stp1)
states: 0
abstracting: (P2<=P4)
states: 35,840 (4)
-> the formula is FALSE

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

MC time: 0m 0.082sec

checking: AG [[[[stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | stp2<=P6] & [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) | 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)<=stp2]] | [[1<=sum(WeightPossibleVal_off, WeightPossibleVal_on) & 2<=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)] | [P1<=stp5 & P4<=P3]]]]
normalized: ~ [E [true U ~ [[[[1<=sum(WeightPossibleVal_off, WeightPossibleVal_on) & 2<=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)] | [P1<=stp5 & P4<=P3]] | [[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) | 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)<=stp2] & [stp2<=sum(WeightPossibleVal_off, WeightPossibleVal_on) | stp2<=P6]]]]]]

abstracting: (stp2<=P6)
states: 33,299 (4)
abstracting: (stp2<=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)<=stp2)
states: 15,523 (4)
abstracting: (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))
states: 43,463 (4)
abstracting: (P4<=P3)
states: 43,342 (4)
abstracting: (P1<=stp5)
states: 22,673 (4)
abstracting: (2<=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: (1<=sum(WeightPossibleVal_off, WeightPossibleVal_on))
states: 43,463 (4)
-> the formula is TRUE

FORMULA AirplaneLD-COL-0010-ReachabilityCardinality-8 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.356sec

totally nodes used: 13171(1.3e+04)
number of garbage collections: 0
fire ops cache: hits/miss/sum: 9386 20998 30384
used/not used/entry size/cache size: 18380 67090484 16 1024MB
basic ops cache: hits/miss/sum: 8117 16832 24949
used/not used/entry size/cache size: 28499 16748717 12 192MB
unary ops cache: hits/miss/sum: 0 703 703
used/not used/entry size/cache size: 703 8387905 8 64MB
abstract ops cache: hits/miss/sum: 0 25184001 25184001
used/not used/entry size/cache size: 42 8388566 12 96MB
state nr cache: hits/miss/sum: 342 497 839
used/not used/entry size/cache size: 497 2096655 32 64MB
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 67095693
1 13171
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
>= 10 0

Total processing time: 0m 7.105sec


BK_STOP 1494883777017

--------------------
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

.......................

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="S_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"

# 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/S_AirplaneLD-PT-0010.tgz
mv S_AirplaneLD-PT-0010 execution

# this is for BenchKit: explicit launching of the test

cd execution
echo "====================================================================="
echo " Generated by BenchKit 2-3254"
echo " Executing tool marcie"
echo " Input is S_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 r081-csrt-149441064000061"
echo "====================================================================="
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
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 ;