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-COL-0010, examination is ReachabilityCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r209su-blw3-146445824100007
=====================================================================

--------------------
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 1464674233445


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=ReachabilityCardinality.xml --mcc-mode --memory=6 --suppress

parse successfull
net created successfully

Unfolding complete |P|=89|T|=88|A|=333
Time for unfolding: 0m 1.008sec

Net: AirplaneLD_COL_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 3.204sec


RS generation: 0m 0.026sec


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



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

checking: AG [~ [3<=stp3_dot]]
normalized: ~ [E [true U 3<=stp3_dot]]

abstracting: (3<=stp3_dot) states: 0
-> the formula is TRUE

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

MC time: 0m 0.000sec

checking: EF [2<=stp1_dot]
normalized: E [true U 2<=stp1_dot]

abstracting: (2<=stp1_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 0.000sec

checking: EF [~ [~ [~ [P4_dot<=stp1_dot]]]]
normalized: E [true U ~ [P4_dot<=stp1_dot]]

abstracting: (P4_dot<=stp1_dot) states: 43,342 (4)
-> the formula is TRUE

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

MC time: 0m 0.022sec

checking: EF [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P6_dot]
normalized: E [true U sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P6_dot]

abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P6_dot) states: 0
-> the formula is FALSE

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

MC time: 0m 0.034sec

checking: AG [[~ [3<=stp1_dot] | ~ [~ [stp4_dot<=stp3_dot]]]]
normalized: ~ [E [true U ~ [[stp4_dot<=stp3_dot | ~ [3<=stp1_dot]]]]]

abstracting: (3<=stp1_dot) states: 0
abstracting: (stp4_dot<=stp3_dot) states: 39,701 (4)
-> the formula is TRUE

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

MC time: 0m 0.000sec

checking: EF [[P5_dot<=stp4_dot & 2<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)]]
normalized: E [true U [P5_dot<=stp4_dot & 2<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)]]

abstracting: (2<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)) states: 0
abstracting: (P5_dot<=stp4_dot) states: 43,452 (4)
-> the formula is FALSE

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

MC time: 0m 0.034sec

checking: EF [~ [[[1<=stp1_dot | P2_dot<=P1_dot] | ~ [2<=P1_dot]]]]
normalized: E [true U ~ [[~ [2<=P1_dot] | [1<=stp1_dot | P2_dot<=P1_dot]]]]

abstracting: (P2_dot<=P1_dot) states: 35,840 (4)
abstracting: (1<=stp1_dot) states: 7,623 (3)
abstracting: (2<=P1_dot) states: 0
-> the formula is FALSE

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

MC time: 0m 0.001sec

checking: AG [[P5_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | 3<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]
normalized: ~ [E [true U ~ [[P5_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | 3<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]]]

abstracting: (3<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)) states: 0
abstracting: (P5_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)) states: 43,452 (4)
-> the formula is FALSE

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

MC time: 0m 0.107sec

checking: EF [~ [3<=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 ~ [3<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]]

abstracting: (3<=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-11 FALSE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 0.033sec

checking: EF [~ [[[1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) | sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=stp5_dot] & ~ [3<=stp3_dot]]]]
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) | sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=stp5_dot] & ~ [3<=stp3_dot]]]]

abstracting: (3<=stp3_dot) states: 0
abstracting: (sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=stp5_dot) states: 34,101 (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)
-> the formula is FALSE

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

MC time: 0m 0.065sec

checking: EF [[[[2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) & 3<=stp5_dot] & [2<=P4_dot | 2<=P1_dot]] & [~ [2<=P2_dot] | ~ [stp4_dot<=stp1_dot]]]]
normalized: E [true U [[~ [2<=P2_dot] | ~ [stp4_dot<=stp1_dot]] & [[2<=P4_dot | 2<=P1_dot] & [2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) & 3<=stp5_dot]]]]

abstracting: (3<=stp5_dot) states: 0
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<=P1_dot) states: 0
abstracting: (2<=P4_dot) states: 0
abstracting: (stp4_dot<=stp1_dot) states: 40,207 (4)
abstracting: (2<=P2_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 0.034sec

checking: EF [~ [[~ [stp1_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<=stp5_dot | 1<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]]]
normalized: E [true U ~ [[~ [stp1_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<=stp5_dot | 1<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)]]]]

abstracting: (1<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)) states: 15,246 (4)
abstracting: (P4_dot<=stp5_dot) states: 43,353 (4)
abstracting: (stp1_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)
-> the formula is TRUE

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

MC time: 0m 0.981sec

checking: EF [[stp3_dot<=stp2_dot & [[P6_dot<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0) & 2<=stp2_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)]]]]
normalized: E [true U [stp3_dot<=stp2_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)] & [P6_dot<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0) & 2<=stp2_dot]]]]

abstracting: (2<=stp2_dot) states: 0
abstracting: (P6_dot<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)) states: 33,165 (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: (stp3_dot<=stp2_dot) states: 42,011 (4)
-> the formula is FALSE

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

MC time: 0m 0.520sec

checking: EF [[[[stp1_dot<=stp1_dot & 2<=P1_dot] & [2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) | 2<=P4_dot]] & [~ [1<=P6_dot] & [sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=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) | P1_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]]]]
normalized: E [true U [[~ [1<=P6_dot] & [sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=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) | P1_dot<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]] & [[2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1) | 2<=P4_dot] & [stp1_dot<=stp1_dot & 2<=P1_dot]]]]

abstracting: (2<=P1_dot) states: 0
abstracting: (stp1_dot<=stp1_dot) states: 43,463 (4)
abstracting: (2<=P4_dot) states: 0
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<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)) states: 43,463 (4)
abstracting: (sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)<=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: (1<=P6_dot) states: 10,298 (4)
-> the formula is FALSE

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

MC time: 0m 0.110sec

checking: EF [~ [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(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)]]
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(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)]]

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(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: 43,463 (4)
-> the formula is FALSE

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

MC time: 0m 0.654sec

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(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) & ~ [3<=P6_dot]]]
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(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) & ~ [3<=P6_dot]]]]]

abstracting: (3<=P6_dot) states: 0
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(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: 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 0.661sec


Total processing time: 0m 8.792sec


BK_STOP 1464674242265

--------------------
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:298 (3), effective:56 (0)
227
iterations count:1662 (18), effective:343 (3)

iterations count:310 (3), effective:57 (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-COL-0010"
export BK_EXAMINATION="ReachabilityCardinality"
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-COL-0010.tgz
mv AirplaneLD-COL-0010 execution

# this is for BenchKit: explicit launching of the test

cd execution
echo "====================================================================="
echo " Generated by BenchKit 2-2979"
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 r209su-blw3-146445824100007"
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 ;