Execution Chart

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

Trace from the execution

Waiting for the VM to be ready (probing ssh)
........
=====================================================================
Generated by BenchKit 2-2979
Executing tool marcie
Input is AirplaneLD-PT-0010, examination is ReachabilityCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r209su-blw3-146445824500088
=====================================================================

--------------------
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 1464677927625


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

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

net check time: 0m 0.000sec

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

init dd package: 0m 3.977sec


RS generation: 0m 0.031sec


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



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

checking: AG [~ [3<=stp3]]
normalized: ~ [E [true U 3<=stp3]]

abstracting: (3<=stp3) 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]
normalized: E [true U 2<=stp1]

abstracting: (2<=stp1) 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<=stp1]]]]
normalized: E [true U ~ [P4<=stp1]]

abstracting: (P4<=stp1) 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 0.025sec

checking: EF [sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P6]
normalized: E [true U sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P6]

abstracting: (sum(WeightPossibleVal_off, WeightPossibleVal_on)<=P6) states: 0
-> the formula is FALSE

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

MC time: 0m 0.035sec

checking: AG [[~ [3<=stp1] | ~ [~ [stp4<=stp3]]]]
normalized: ~ [E [true U ~ [[stp4<=stp3 | ~ [3<=stp1]]]]]

abstracting: (3<=stp1) states: 0
abstracting: (stp4<=stp3) 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 0.001sec

checking: EF [[P5<=stp4 & 2<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)]]
normalized: E [true U [P5<=stp4 & 2<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)]]

abstracting: (2<=sum(Weight_Right_Wheel_off, Weight_Right_Wheel_on)) states: 0
abstracting: (P5<=stp4) 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 0.033sec

checking: EF [~ [[~ [2<=P1] | [1<=stp1 | P2<=P1]]]]
normalized: E [true U ~ [[[1<=stp1 | P2<=P1] | ~ [2<=P1]]]]

abstracting: (2<=P1) states: 0
abstracting: (P2<=P1) states: 35,840 (4)
abstracting: (1<=stp1) states: 7,623 (3)
-> 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<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | 3<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)]]
normalized: ~ [E [true U ~ [[P5<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T) | 3<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)]]]]

abstracting: (3<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)) states: 0
abstracting: (P5<=sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)) 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 0.113sec

checking: EF [~ [3<=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 ~ [3<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]]

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

MC time: 0m 0.032sec

checking: EF [~ [[[1<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1) | sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=stp5] & ~ [3<=stp3]]]]
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) | sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=stp5] & ~ [3<=stp3]]]]

abstracting: (3<=stp3) states: 0
abstracting: (sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=stp5) states: 34,101 (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)
-> the formula is FALSE

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

MC time: 0m 0.070sec

checking: EF [[[[2<=P1 | 2<=P4] & [3<=stp5 & 2<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]] & [~ [2<=P2] | ~ [stp4<=stp1]]]]
normalized: E [true U [[[2<=P1 | 2<=P4] & [3<=stp5 & 2<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1)]] & [~ [2<=P2] | ~ [stp4<=stp1]]]]

abstracting: (stp4<=stp1) states: 40,207 (4)
abstracting: (2<=P2) states: 0
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: (3<=stp5) states: 0
abstracting: (2<=P4) states: 0
abstracting: (2<=P1) states: 0
-> the formula is FALSE

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

MC time: 0m 0.037sec

checking: EF [~ [[~ [stp1<=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<=stp5 | 1<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)]]]]
normalized: E [true U ~ [[~ [stp1<=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<=stp5 | 1<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)]]]]

abstracting: (1<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)) states: 15,246 (4)
abstracting: (P4<=stp5) states: 43,353 (4)
abstracting: (stp1<=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-9 TRUE TECHNIQUES SEQUENTIAL_PROCESSING DECISION_DIAGRAMS UNFOLDING_TO_PT

MC time: 0m 1.196sec

checking: EF [[stp3<=stp2 & [[P6<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on) & 2<=stp2] & ~ [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)]]]]
normalized: E [true U [stp3<=stp2 & [~ [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)] & [P6<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on) & 2<=stp2]]]]

abstracting: (2<=stp2) states: 0
abstracting: (P6<=sum(Weight_Left_Wheel_off, Weight_Left_Wheel_on)) states: 33,165 (4)
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)
abstracting: (stp3<=stp2) 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 0.575sec

checking: EF [[[[stp1<=stp1 & 2<=P1] & [2<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1) | 2<=P4]] & [~ [1<=P6] & [sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=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) | P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)]]]]
normalized: E [true U [[[sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=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) | P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)] & ~ [1<=P6]] & [[2<=sum(SpeedPossibleVal_10, SpeedPossibleVal_9, SpeedPossibleVal_8, SpeedPossibleVal_7, SpeedPossibleVal_6, SpeedPossibleVal_5, SpeedPossibleVal_4, SpeedPossibleVal_3, SpeedPossibleVal_2, SpeedPossibleVal_1) | 2<=P4] & [stp1<=stp1 & 2<=P1]]]]

abstracting: (2<=P1) states: 0
abstracting: (stp1<=stp1) states: 43,463 (4)
abstracting: (2<=P4) states: 0
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: (1<=P6) states: 10,298 (4)
abstracting: (P1<=sum(WeightPossibleVal_off, WeightPossibleVal_on)) states: 43,463 (4)
abstracting: (sum(Plane_On_Ground_Signal_no_F, Plane_On_Ground_Signal_no_T)<=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)
-> the formula is FALSE

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

MC time: 0m 0.118sec

checking: EF [~ [sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)<=sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)]]
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(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)]]

abstracting: (sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)<=sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)) 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 0.858sec

checking: AG [[~ [3<=P6] & sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)<=sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)]]
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(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1) & ~ [3<=P6]]]]]

abstracting: (3<=P6) states: 0
abstracting: (sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)<=sum(TheAltitude_20, TheAltitude_19, TheAltitude_18, TheAltitude_17, TheAltitude_16, TheAltitude_15, TheAltitude_14, TheAltitude_13, TheAltitude_12, TheAltitude_11, TheAltitude_10, TheAltitude_9, TheAltitude_8, TheAltitude_7, TheAltitude_6, TheAltitude_5, TheAltitude_4, TheAltitude_3, TheAltitude_2, TheAltitude_1)) states: 43,463 (4)
-> the formula is TRUE

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

MC time: 0m 0.747sec


Total processing time: 0m 9.245sec


BK_STOP 1464677936902

--------------------
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-PT-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-PT-0010.tgz
mv AirplaneLD-PT-0010 execution

# this is for BenchKit: explicit launching of the test

cd execution
echo "====================================================================="
echo " Generated by BenchKit 2-2979"
echo " Executing tool marcie"
echo " Input is AirplaneLD-PT-0010, examination is 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-blw3-146445824500088"
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 ;