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 AirplaneLD-COL-0010, examination is ReachabilityCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r001-csrt-149436061000007
=====================================================================

--------------------
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 1494448508193

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

Unfolding complete |P|=89|T|=88|A|=333
Time for unfolding: 0m 0.820sec

Net: AirplaneLD_COL_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 1.060sec


RS generation: 0m 0.006sec


-> reachability set: #nodes 190 (1.9e+02) #states 43,463 (4)



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

checking: EF [~ [~ [3<=stp5_dot]]]
normalized: E [true U 3<=stp5_dot]

abstracting: (3<=stp5_dot)
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_dot]
normalized: E [true U 3<=stp2_dot]

abstracting: (3<=stp2_dot)
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_dot]
normalized: E [true U 2<=stp4_dot]

abstracting: (2<=stp4_dot)
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_dot]
normalized: E [true U 2<=stp2_dot]

abstracting: (2<=stp2_dot)
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_dot & 2<=stp3_dot]]]]
normalized: E [true U [1<=stp1_dot & 2<=stp3_dot]]

abstracting: (2<=stp3_dot)
states: 0
abstracting: (1<=stp1_dot)
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_Weight1, WeightPossibleVal_Weight0) | ~ [~ [1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]]]]
normalized: ~ [E [true U ~ [[2<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | 1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]]]]

abstracting: (1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
states: 43,463 (4)
abstracting: (2<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
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 0.033sec

checking: EF [[[2<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) & ~ [P6_dot<=stp5_dot]] & [[1<=P3_dot | 1<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)] | [1<=stp5_dot & 3<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]]]
normalized: E [true U [[[1<=stp5_dot & 3<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)] | [1<=P3_dot | 1<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]] & [~ [P6_dot<=stp5_dot] & 2<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]

abstracting: (2<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 0
abstracting: (P6_dot<=stp5_dot)
states: 34,101 (4)
abstracting: (1<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 10,298 (4)
abstracting: (1<=P3_dot)
states: 2,541 (3)
abstracting: (3<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0))
states: 0
abstracting: (1<=stp5_dot)
states: 3,951 (3)
-> the formula is FALSE

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

MC time: 0m 0.051sec

checking: EF [~ [1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]]
normalized: E [true U ~ [1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]]

abstracting: (1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1))
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 0.016sec

checking: EF [[1<=P3_dot | [[sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=P4_dot | sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P1_dot] & [3<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | 3<=P2_dot]]]]
normalized: E [true U [1<=P3_dot | [[3<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | 3<=P2_dot] & [sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=P4_dot | sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P1_dot]]]]

abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P1_dot)
states: 0
abstracting: (sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=P4_dot)
states: 4,083 (3)
abstracting: (3<=P2_dot)
states: 0
abstracting: (3<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0))
states: 0
abstracting: (1<=P3_dot)
states: 2,541 (3)
-> the formula is TRUE

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

MC time: 0m 0.056sec

checking: EF [[[[sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0) | 2<=stp1_dot] & P6_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)] & ~ [[2<=P4_dot & 3<=stp2_dot]]]]
normalized: E [true U [~ [[2<=P4_dot & 3<=stp2_dot]] & [P6_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1) & [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0) | 2<=stp1_dot]]]]

abstracting: (2<=stp1_dot)
states: 0
abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0))
states: 0
abstracting: (P6_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 42,525 (4)
abstracting: (3<=stp2_dot)
states: 0
abstracting: (2<=P4_dot)
states: 0
-> the formula is FALSE

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

MC time: 0m 0.036sec

checking: EF [~ [[[P1_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | 2<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)] | 2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]]]
normalized: E [true U ~ [[[P1_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | 2<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)] | 2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]]]

abstracting: (2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1))
states: 43,463 (4)
abstracting: (2<=sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1))
states: 0
abstracting: (P1_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
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 0.047sec

checking: EF [[[~ [2<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)] & ~ [2<=stp3_dot]] & [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=stp2_dot & 2<=P4_dot]]]
normalized: E [true U [[~ [2<=stp3_dot] & ~ [2<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]] & [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=stp2_dot & 2<=P4_dot]]]

abstracting: (2<=P4_dot)
states: 0
abstracting: (sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=stp2_dot)
states: 33,299 (4)
abstracting: (2<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1))
states: 43,463 (4)
abstracting: (2<=stp3_dot)
states: 0
-> the formula is FALSE

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

MC time: 0m 0.031sec

checking: EF [[[[1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) | P3_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)] & ~ [2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]] & [[P2_dot<=stp2_dot & P1_dot<=P5_dot] & [2<=P1_dot & 2<=P1_dot]]]]
normalized: E [true U [[[2<=P1_dot & 2<=P1_dot] & [P2_dot<=stp2_dot & P1_dot<=P5_dot]] & [~ [2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)] & [1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) | P3_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)]]]]

abstracting: (P3_dot<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 43,232 (4)
abstracting: (1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1))
states: 43,463 (4)
abstracting: (2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1))
states: 43,463 (4)
abstracting: (P1_dot<=P5_dot)
states: 20,594 (4)
abstracting: (P2_dot<=stp2_dot)
states: 38,381 (4)
abstracting: (2<=P1_dot)
states: 0
abstracting: (2<=P1_dot)
states: 0
-> the formula is FALSE

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

MC time: 0m 0.024sec

checking: AG [sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]
normalized: ~ [E [true U ~ [sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)]]]

abstracting: (sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1))
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 0.510sec

checking: EF [[P2_dot<=P4_dot & [[sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=P4_dot & 3<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)] | [sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp1_dot | sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp3_dot]]]]
normalized: E [true U [P2_dot<=P4_dot & [[sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp1_dot | sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp3_dot] | [sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=P4_dot & 3<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1)]]]]

abstracting: (3<=sum(Speed_Right_Wheel_Speed9, Speed_Right_Wheel_Speed8, Speed_Right_Wheel_Speed7, Speed_Right_Wheel_Speed6, Speed_Right_Wheel_Speed5, Speed_Right_Wheel_Speed4, Speed_Right_Wheel_Speed3, Speed_Right_Wheel_Speed2, Speed_Right_Wheel_Speed10, Speed_Right_Wheel_Speed1))
states: 0
abstracting: (sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1)<=P4_dot)
states: 0
abstracting: (sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp3_dot)
states: 0
abstracting: (sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp1_dot)
states: 0
abstracting: (P2_dot<=P4_dot)
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 0.064sec

checking: AG [[[[1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) & 2<=sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)] | [P1_dot<=stp5_dot & P4_dot<=P3_dot]] | [[stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | stp2_dot<=P6_dot] & [P1_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1) | sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=stp2_dot]]]]
normalized: ~ [E [true U ~ [[[[stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) | stp2_dot<=P6_dot] & [P1_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1) | sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=stp2_dot]] | [[1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0) & 2<=sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1)] | [P1_dot<=stp5_dot & P4_dot<=P3_dot]]]]]]

abstracting: (P4_dot<=P3_dot)
states: 43,342 (4)
abstracting: (P1_dot<=stp5_dot)
states: 22,673 (4)
abstracting: (2<=sum(TheAltitude_Altitude9, TheAltitude_Altitude8, TheAltitude_Altitude7, TheAltitude_Altitude6, TheAltitude_Altitude5, TheAltitude_Altitude4, TheAltitude_Altitude3, TheAltitude_Altitude20, TheAltitude_Altitude2, TheAltitude_Altitude19, TheAltitude_Altitude18, TheAltitude_Altitude17, TheAltitude_Altitude16, TheAltitude_Altitude15, TheAltitude_Altitude14, TheAltitude_Altitude13, TheAltitude_Altitude12, TheAltitude_Altitude11, TheAltitude_Altitude10, TheAltitude_Altitude1))
states: 0
abstracting: (1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
states: 43,463 (4)
abstracting: (sum(Speed_Left_Wheel_Speed9, Speed_Left_Wheel_Speed8, Speed_Left_Wheel_Speed7, Speed_Left_Wheel_Speed6, Speed_Left_Wheel_Speed5, Speed_Left_Wheel_Speed4, Speed_Left_Wheel_Speed3, Speed_Left_Wheel_Speed2, Speed_Left_Wheel_Speed10, Speed_Left_Wheel_Speed1)<=stp2_dot)
states: 15,523 (4)
abstracting: (P1_dot<=sum(AltitudePossibleVal_Altitude9, AltitudePossibleVal_Altitude8, AltitudePossibleVal_Altitude7, AltitudePossibleVal_Altitude6, AltitudePossibleVal_Altitude5, AltitudePossibleVal_Altitude4, AltitudePossibleVal_Altitude3, AltitudePossibleVal_Altitude20, AltitudePossibleVal_Altitude2, AltitudePossibleVal_Altitude19, AltitudePossibleVal_Altitude18, AltitudePossibleVal_Altitude17, AltitudePossibleVal_Altitude16, AltitudePossibleVal_Altitude15, AltitudePossibleVal_Altitude14, AltitudePossibleVal_Altitude13, AltitudePossibleVal_Altitude12, AltitudePossibleVal_Altitude11, AltitudePossibleVal_Altitude10, AltitudePossibleVal_Altitude1))
states: 43,463 (4)
abstracting: (stp2_dot<=P6_dot)
states: 33,299 (4)
abstracting: (stp2_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0))
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 0.278sec

totally nodes used: 26668(2.7e+04)
number of garbage collections: 0
fire ops cache: hits/miss/sum: 11386 43959 55345
used/not used/entry size/cache size: 41133 67067731 16 1024MB
basic ops cache: hits/miss/sum: 9987 33322 43309
used/not used/entry size/cache size: 64930 16712286 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 2252903 2252903
used/not used/entry size/cache size: 78 8388530 12 96MB
state nr cache: hits/miss/sum: 799 1903 2702
used/not used/entry size/cache size: 1903 2095249 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 67082198
1 26664
2 2
3 0
4 0
5 0
6 0
7 0
8 0
9 0
>= 10 0

Total processing time: 0m 3.548sec


BK_STOP 1494448511777

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

check for maximal unmarked siphon
ok
check for constant places
AltitudePossibleVal_Altitude1
AltitudePossibleVal_Altitude2
AltitudePossibleVal_Altitude3
AltitudePossibleVal_Altitude4
AltitudePossibleVal_Altitude5
AltitudePossibleVal_Altitude6
AltitudePossibleVal_Altitude7
AltitudePossibleVal_Altitude8
AltitudePossibleVal_Altitude9
AltitudePossibleVal_Altitude10
AltitudePossibleVal_Altitude11
AltitudePossibleVal_Altitude12
AltitudePossibleVal_Altitude13
AltitudePossibleVal_Altitude14
AltitudePossibleVal_Altitude15
AltitudePossibleVal_Altitude16
AltitudePossibleVal_Altitude17
AltitudePossibleVal_Altitude18
AltitudePossibleVal_Altitude19
AltitudePossibleVal_Altitude20
SpeedPossibleVal_Speed1
SpeedPossibleVal_Speed2
SpeedPossibleVal_Speed3
SpeedPossibleVal_Speed4
SpeedPossibleVal_Speed5
SpeedPossibleVal_Speed6
SpeedPossibleVal_Speed7
SpeedPossibleVal_Speed8
SpeedPossibleVal_Speed9
SpeedPossibleVal_Speed10
WeightPossibleVal_Weight0
WeightPossibleVal_Weight1
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="AirplaneLD-COL-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/AirplaneLD-COL-0010.tgz
mv AirplaneLD-COL-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 AirplaneLD-COL-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-csrt-149436061000007"
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 ;