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 CTLCardinality
Time confinement is 3600 seconds
Memory confinement is 16384 MBytes
Number of cores is 1
Run identifier is r209su-blw3-146445824100003
=====================================================================

--------------------
content from stdout:

=== Data for post analysis generated by BenchKit (invocation template)

The expected result is a vector of booleans
BOOL_VECTOR

here is the order used to build the result vector(from text file)
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-0
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-1
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-10
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-11
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-12
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-13
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-14
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-15
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-2
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-3
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-4
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-5
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-6
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-7
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-8
FORMULA_NAME AirplaneLD-COL-0010-CTLCardinality-9

=== Now, execution of the tool begins

BK_START 1464674236661


Marcie rev. 8535M (built: crohr on 2016-04-27)
A model checker for Generalized Stochastic Petri nets

authors: Alex Tovchigrechko (IDD package and CTL model checking)

Martin Schwarick (Symbolic numerical analysis and CSL model checking)

Christian Rohr (Simulative and approximative numerical model checking)

marcie@informatik.tu-cottbus.de

called as: marcie --net-file=model.pnml --mcc-file=CTLCardinality.xml --mcc-mode --memory=6 --suppress

parse successfull
net created successfully

Unfolding complete |P|=89|T|=88|A|=333
Time for unfolding: 0m 1.133sec

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 3.500sec


RS generation: 0m 0.025sec


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



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

checking: ~ [~ [AG [P3_dot<=stp1_dot]]]
normalized: ~ [E [true U ~ [P3_dot<=stp1_dot]]]

abstracting: (P3_dot<=stp1_dot) states: 40,922 (4)
-> the formula is FALSE

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

MC time: 0m 0.006sec

checking: AG [1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]
normalized: ~ [E [true U ~ [1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)]]]

abstracting: (1<=sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)) states: 43,463 (4)
-> the formula is TRUE

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

MC time: 0m 0.027sec

checking: ~ [AG [AX [P4_dot<=stp5_dot]]]
normalized: E [true U EX [~ [P4_dot<=stp5_dot]]]

abstracting: (P4_dot<=stp5_dot) states: 43,353 (4)
.-> the formula is TRUE

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

MC time: 0m 0.022sec

checking: AF [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P3_dot]
normalized: ~ [EG [~ [sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P3_dot]]]

abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=P3_dot) states: 0

EG iterations: 0
-> the formula is FALSE

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

MC time: 0m 0.029sec

checking: [EF [~ [[1<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0) & 2<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]] & EG [[P6_dot<=P2_dot | 2<=P1_dot]]]
normalized: [E [true U ~ [[1<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0) & 2<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]] & EG [[P6_dot<=P2_dot | 2<=P1_dot]]]

abstracting: (2<=P1_dot) states: 0
abstracting: (P6_dot<=P2_dot) states: 33,165 (4)
...........
EG iterations: 11
abstracting: (2<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)) states: 0
abstracting: (1<=sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)) states: 15,246 (4)
-> the formula is FALSE

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

MC time: 0m 0.120sec

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

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

MC time: 0m 0.055sec

checking: EX [EG [[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) | 1<=stp3_dot]]]
normalized: EX [EG [[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) | 1<=stp3_dot]]]

abstracting: (1<=stp3_dot) states: 2,057 (3)
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)
.......
EG iterations: 7
.-> the formula is TRUE

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

MC time: 0m 0.066sec

checking: AG [[EX [stp2_dot<=P4_dot] | ~ [[1<=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) | 3<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)]]]]
normalized: ~ [E [true U ~ [[~ [[1<=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) | 3<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)]] | EX [stp2_dot<=P4_dot]]]]]

abstracting: (stp2_dot<=P4_dot) states: 30,758 (4)
.abstracting: (3<=sum(Weight_Right_Wheel_Weight1, Weight_Right_Wheel_Weight0)) states: 0
abstracting: (1<=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: 39,490 (4)
-> the formula is FALSE

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

MC time: 0m 0.107sec

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

EG iterations: 0
-> the formula is FALSE

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

MC time: 0m 0.033sec

checking: EF [~ [AF [stp2_dot<=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 EG [~ [stp2_dot<=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: (stp2_dot<=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: 42,858 (4)
......
EG iterations: 6
-> the formula is FALSE

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

MC time: 0m 0.947sec

checking: ~ [[AG [~ [sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp5_dot]] & A [1<=stp2_dot U 1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]]]
normalized: ~ [[[~ [EG [~ [1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]]] & ~ [E [~ [1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)] U [~ [1<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)] & ~ [1<=stp2_dot]]]]] & ~ [E [true U sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp5_dot]]]]

abstracting: (sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)<=stp5_dot) states: 0
abstracting: (1<=stp2_dot) states: 12,705 (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: (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: (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)
.
EG iterations: 1
-> the formula is FALSE

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

MC time: 0m 0.120sec

checking: EG [[EX [P2_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)] & EF [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=P6_dot]]]
normalized: EG [[EX [P2_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)] & E [true U sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=P6_dot]]]

abstracting: (sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=P6_dot) states: 28,217 (4)
abstracting: (P2_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)
............
EG iterations: 11
-> the formula is FALSE

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

MC time: 0m 1.033sec

checking: [~ [[AG [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=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)<=P6_dot]]] & [~ [1<=stp3_dot] | P3_dot<=stp3_dot]]
normalized: [~ [[~ [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)<=P6_dot] | ~ [E [true U ~ [sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=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)]]]]] & [P3_dot<=stp3_dot | ~ [1<=stp3_dot]]]

abstracting: (1<=stp3_dot) states: 2,057 (3)
abstracting: (P3_dot<=stp3_dot) states: 41,043 (4)
abstracting: (sum(Weight_Left_Wheel_Weight1, Weight_Left_Wheel_Weight0)<=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: (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)<=P6_dot) states: 13,323 (4)
-> the formula is FALSE

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

MC time: 0m 1.931sec

checking: [[~ [~ [~ [1<=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<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | P2_dot<=P4_dot] | ~ [3<=stp1_dot]] & AF [2<=stp3_dot]]] & ~ [1<=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: [[~ [1<=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)] | [~ [EG [~ [2<=stp3_dot]]] & [~ [3<=stp1_dot] | [2<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0) | P2_dot<=P4_dot]]]] & ~ [1<=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: (1<=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: 41,140 (4)
abstracting: (P2_dot<=P4_dot) states: 35,840 (4)
abstracting: (2<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)) states: 0
abstracting: (3<=stp1_dot) states: 0
abstracting: (2<=stp3_dot) states: 0

EG iterations: 0
abstracting: (1<=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 FALSE

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

MC time: 0m 1.012sec

checking: [EF [[[P4_dot<=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<=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)] & [P2_dot<=P3_dot | stp2_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]] & AG [[[P3_dot<=P6_dot & P6_dot<=stp4_dot] | ~ [3<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]
normalized: [~ [E [true U ~ [[[P3_dot<=P6_dot & P6_dot<=stp4_dot] | ~ [3<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)]]]]] & E [true U [[P2_dot<=P3_dot | stp2_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)] & [P4_dot<=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<=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: (3<=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: (P4_dot<=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: 43,342 (4)
abstracting: (stp2_dot<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)) states: 33,299 (4)
abstracting: (P2_dot<=P3_dot) states: 35,840 (4)
abstracting: (3<=sum(Plane_On_Ground_Signal_no_Signal1, Plane_On_Ground_Signal_no_Signal0)) states: 0
abstracting: (P6_dot<=stp4_dot) states: 34,100 (4)
abstracting: (P3_dot<=P6_dot) states: 40,922 (4)
-> the formula is FALSE

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

MC time: 0m 1.565sec

checking: E [[[3<=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(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=stp3_dot] | ~ [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)<=stp2_dot]] U EG [2<=sum(SpeedPossibleVal_Speed9, SpeedPossibleVal_Speed8, SpeedPossibleVal_Speed7, SpeedPossibleVal_Speed6, SpeedPossibleVal_Speed5, SpeedPossibleVal_Speed4, SpeedPossibleVal_Speed3, SpeedPossibleVal_Speed2, SpeedPossibleVal_Speed10, SpeedPossibleVal_Speed1)]]
normalized: E [[~ [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)<=stp2_dot] | [3<=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(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=stp3_dot]] U EG [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)

EG iterations: 0
abstracting: (sum(WeightPossibleVal_Weight1, WeightPossibleVal_Weight0)<=stp3_dot) states: 0
abstracting: (3<=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: (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)<=stp2_dot) states: 14,423 (4)
-> the formula is TRUE

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

MC time: 0m 1.532sec


Total processing time: 0m14.483sec


BK_STOP 1464674251177

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

check for maximal unmarked siphon
ok
check if there are places and transitions
ok
check if there are transitions without pre-places
ok
check if at least one transition is enabled in m0
ok
check if there are transitions that can never fire
ok


initing FirstDep: 0m 0.000sec

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

initing FirstDep: 0m 0.000sec


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

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

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

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

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

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

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

Sequence of Actions to be Executed by the VM

This is useful if one wants to reexecute the tool in the VM from the submitted image disk.

set -x
# this is for BenchKit: configuration of major elements for the test
export BK_INPUT="AirplaneLD-COL-0010"
export BK_EXAMINATION="CTLCardinality"
export BK_TOOL="marcie"
export BK_RESULT_DIR="/home/hulinhub/BK_RESULTS/OUTPUTS"
export BK_TIME_CONFINEMENT="3600"
export BK_MEMORY_CONFINEMENT="16384"

# this is specific to your benchmark or test

export BIN_DIR="$HOME/BenchKit/bin"

# remove the execution directoty if it exists (to avoid increse of .vmdk images)
if [ -d execution ] ; then
rm -rf execution
fi

tar xzf /home/mcc/BenchKit/INPUTS/AirplaneLD-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 CTLCardinality"
echo " Time confinement is $BK_TIME_CONFINEMENT seconds"
echo " Memory confinement is 16384 MBytes"
echo " Number of cores is 1"
echo " Run identifier is r209su-blw3-146445824100003"
echo "====================================================================="
echo
echo "--------------------"
echo "content from stdout:"
echo
echo "=== Data for post analysis generated by BenchKit (invocation template)"
echo
if [ "CTLCardinality" = "UpperBounds" ] ; then
echo "The expected result is a vector of positive values"
echo NUM_VECTOR
elif [ "CTLCardinality" != "StateSpace" ] ; then
echo "The expected result is a vector of booleans"
echo BOOL_VECTOR
else
echo "no data necessary for post analysis"
fi
echo
if [ -f "CTLCardinality.txt" ] ; then
echo "here is the order used to build the result vector(from text file)"
for x in $(grep Property CTLCardinality.txt | cut -d ' ' -f 2 | sort -u) ; do
echo "FORMULA_NAME $x"
done
elif [ -f "CTLCardinality.xml" ] ; then # for cunf (txt files deleted;-)
echo echo "here is the order used to build the result vector(from xml file)"
for x in $(grep '' CTLCardinality.xml | cut -d '>' -f 2 | cut -d '<' -f 1 | sort -u) ; do
echo "FORMULA_NAME $x"
done
fi
echo
echo "=== Now, execution of the tool begins"
echo
echo -n "BK_START "
date -u +%s%3N
echo
timeout -s 9 $BK_TIME_CONFINEMENT bash -c "/home/mcc/BenchKit/BenchKit_head.sh 2> STDERR ; echo ; echo -n \"BK_STOP \" ; date -u +%s%3N"
if [ $? -eq 137 ] ; then
echo
echo "BK_TIME_CONFINEMENT_REACHED"
fi
echo
echo "--------------------"
echo "content from stderr:"
echo
cat STDERR ;