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Transcript of Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical...
![Page 1: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/1.jpg)
Integration of EASY5/GSDSfor Auto Code Generation and Testing
Mike Bingle, Associate Technical Fellow
Model Based Processes and Tools
Simulation Engineering
The Boeing Commercial Airplane Group
![Page 2: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/2.jpg)
2
Discussion TopicsDiscussion Topics
Boeing Commercial Airplane Group model based process
– A bit of background to our work
– A brief overview of GSDS and how auto code generation is
applied
Easy5/GSDS Integration
– What problem are we solving?
Low Level Functions Project
– A first application
Conclusion
– Some final words
![Page 3: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/3.jpg)
3
Discussion TopicsDiscussion Topics
Boeing Commercial Airplane Group model based process
– A bit of background to our work
– A brief overview of GSDS and how auto code generation is
applied
Easy5/GSDS Integration
– What problem are we solving?
Low Level Functions Project
– A first application
Conclusion
– Some final words
![Page 4: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/4.jpg)
4
Model UsageModel Usage
LRU FunctionalRequirements
TrainingSimulators
Airplane LevelEngineering
Model
Model Developers
EngineeringAnalysis/Simulation
IntegrationLabs
Systems &Operational
Training
ModelRepository
![Page 5: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/5.jpg)
5
GSDS OverviewGSDS Overview
SUBROUTINE autotC --------------------------------------------------------------- *C BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET *C Copyright (C) 1998, The Boeing Company *C Unpublished Work -- All Rights Reserved *C --------------------------------------------------------------- *C ORIGIN : Generated by BDED version K00.1 *C Created on 16:21:48 04/09/1998 *C PROCESS NAME : autot *C PROCESS NUMBER: 1.1.4 *C PARENT PROCESS: air_sys *C GENERATED : 14:00:21 05/01/1998 *C AUTHOR : *C --------------------------------------------------------------- *C PREAMBLE: *C *C Automatic throttle *C *C --------------------------------------------------------------- *C ARGUMENT DECLARATIONS: *C --------------------------------------------------------------- *CC --------------------------------------------------------------- *C DECLARATIONS FOR USER DEFINED LOCAL CONSTANTS: *C --------------------------------------------------------------- *C *C *C --------------------------------------------------------------- *C COMMON DEFINITIONS: *C --------------------------------------------------------------- *%NOLIST%include 'inc/sxcom_in.fc'%include 'inc/sxcom.fc'%include 'inc/aero_out.fc'%include 'inc/eom_cmn.fc'%include 'inc/autot_cmn.fc'%include 'inc/modefl.fc'%include 'inc/deltco.fc'%LISTC --------------------------------------------------------------- *C MAINTAIN STATUS OF ALL ENTITIES *C * SAVEC --------------------------------------------------------------- *
C --------------------------------------------------------------- *C DECLARATIONS FOR USER DEFINED LOCAL VARIABLES: *C --------------------------------------------------------------- *C --------------------------------------------------------------- *C DATA STATEMENTS FOR USER DEFINED LOCAL VARIABLES: *C --------------------------------------------------------------- *C --------------------------------------------------------------- *C DECLARATIONS FOR GENERATED LOCAL VARIABLES: *C --------------------------------------------------------------- * REAL q002 { In autot on io between block 8 and 9. REAL rinp000 { In autot with block 8 REAL rout001 { In autot with block 8C --------------------------------------------------------------- *CC DECLARATIONS FOR FUNCTIONS: *C * REAL ALIMIT REAL INTRAPC --------------------------------------------------------------- *C *C FUNCTION INCLUDE FILES: *C *C *C --------------------------------------------------------------- *C PROGRAM: *C --------------------------------------------------------------- *C --------------------------------------------------------------- *C PROCESS autot 1.1.4C --------------------------------------------------------------- * q002 = INTRAP(((sxvcom * kntfps) - vtsx - (udotsx * gain1t))* & gain2t, imoden, to2, tlaic, rinp000, rout001) tla = ALIMIT(q002, 0.0, 100.0)C --------------------------------------------------------------- *C END autot 1.1.4C --------------------------------------------------------------- *
RETURN END
![Page 6: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/6.jpg)
6
Simulation - BackgroundSimulation - Background
Produce large scale simulations for Boeing airplanes
– 707, 727, 737, 747, 757, 767, 777
~500K lines of FORTRAN per airplane model with a staff of 100
engineers, the 777 has over 1M lines of code
Modeling of the following types
– Aerodynamic flight characteristics
– Avionics & flight controls units
– Propulsion, mechanical & electrical systems
Simulations execute on high-end HP 9000 servers & Concurrent
NightHawk real-time computers
![Page 7: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/7.jpg)
7
Simulation - UsageSimulation - Usage
Interactive Use (No Airplane H/W)– Engineering Studies– Simulation Development– Simulator data documents
Engineering Flight Deck Simulators
– Engineering studies
– Pilot evaluation
– Accident/incident investigation
Avionics/Flight Control Test Benches– Airplane system testing
![Page 8: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/8.jpg)
8
Discussion TopicsDiscussion Topics
Boeing Commercial Airplane Group model based process
– A bit of background to our work
GSDS & Auto Code Generation in simulation development
– A brief overview of GSDS and how auto code generation is applied
Easy5/GSDS Integration
– What problem are we solving?
Low Level Functions Project
– A first application
Conclusion
– Some final words
![Page 9: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/9.jpg)
9
What Problem are we Solving?What Problem are we Solving?
Model Developers
EngineeringAnalysis/Simulation
ModelRepository
SUBROUTINE autotC --------------------------------------------------------------- *C BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET *C Copyright (C) 1998, The Boeing Company *C Unpublished Work -- All Rights Reserved *C --------------------------------------------------------------- *C ORIGIN : Generated by BDED version K00.1 *C Created on 16:21:48 04/09/1998 *C PROCESS NAME : autot *C PROCESS NUMBER: 1.1.4 *C PARENT PROCESS: air_sys *C GENERATED : 14:00:21 05/01/1998 *C AUTHOR : *C --------------------------------------------------------------- *C PREAMBLE: *C *C Automatic throttle *C *C --------------------------------------------------------------- *C ARGUMENT DECLARATIONS: *C --------------------------------------------------------------- *CC --------------------------------------------------------------- *C DECLARATIONS FOR USER DEFINED LOCAL CONSTANTS: *C --------------------------------------------------------------- *C *C *C --------------------------------------------------------------- *C COMMON DEFINITIONS: *C --------------------------------------------------------------- *%NOLIST%include 'inc/sxcom_in.fc'%include 'inc/sxcom.fc'%include 'inc/aero_out.fc'%include 'inc/eom_cmn.fc'%include 'inc/autot_cmn.fc'%include 'inc/modefl.fc'%include 'inc/deltco.fc'%LISTC --------------------------------------------------------------- *C MAINTAIN STATUS OF ALL ENTITIES *C * SAVEC --------------------------------------------------------------- *
C --------------------------------------------------------------- *C DECLARATIONS FOR USER DEFINED LOCAL VARIABLES: *C --------------------------------------------------------------- *C --------------------------------------------------------------- *C DATA STATEMENTS FOR USER DEFINED LOCAL VARIABLES: *C --------------------------------------------------------------- *C --------------------------------------------------------------- *C DECLARATIONS FOR GENERATED LOCAL VARIABLES: *C --------------------------------------------------------------- * REAL q002 { In autot on io between block 8 and 9. REAL rinp000 { In autot with block 8 REAL rout001 { In autot with block 8C --------------------------------------------------------------- *CC DECLARATIONS FOR FUNCTIONS: *C * REAL ALIMIT REAL INTRAPC --------------------------------------------------------------- *C *C FUNCTION INCLUDE FILES: *C *C *C --------------------------------------------------------------- *C PROGRAM: *C --------------------------------------------------------------- *C --------------------------------------------------------------- *C PROCESS autot 1.1.4C --------------------------------------------------------------- * q002 = INTRAP(((sxvcom * kntfps) - vtsx - (udotsx * gain1t))* & gain2t, imoden, to2, tlaic, rinp000, rout001) tla = ALIMIT(q002, 0.0, 100.0)C --------------------------------------------------------------- *C END autot 1.1.4C --------------------------------------------------------------- *
RETURN END
Specification, Code Generation andLarge Scale Simulation
Analysis and Small Scale Simulation
Two forms of the same model!
![Page 10: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/10.jpg)
10
Discussion TopicsDiscussion Topics
Boeing Commercial Airplane Group model based process
– A bit of background to our work
GSDS & Auto Code Generation in simulation development
– A brief overview of GSDS and how auto code generation is applied
Easy5/GSDS Integration
– What problem are we solving?
Low Level Functions Project
– A first application
Conclusion
– Some final words
![Page 11: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/11.jpg)
11
Model UsageModel Usage
LRU FunctionalRequirements
TrainingSimulators
Airplane LevelEngineering
Model
Model Developers
EngineeringAnalysis/Simulation
IntegrationLabs
Systems &Operational
Training
ModelRepository
![Page 12: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/12.jpg)
12
Low Level Functions ProjectLow Level Functions Project
Objective
– Enable reuse of BCAG developed models by LRU suppliers and Training Simulator Manufacturers
(4*184.5)
Honeywell
Boeing
pvsgmdpvscmdwmspd
pvsgn
vertspd209:22:24 08/29/1996Layer: 4
FIGURE 1.4.2-1 Vertical SpeedRef: D6-37704, Fig.2-29, Pg 2-67
*
*- LRU Only
IN
SYMMETRICAL LIMIT
Note: This page is only called when in either MCP orVNAV Vertical Speed modes (i.e., 128 is onlywritten into SCMODE in VNAV Vertical Speed.)
L
DD
N
IC
IC
IC
A
RS
TAU
H
L
N
N
D
A
A
B
B
BA
RSET
RSET
B
AL
SL
hold_fcc
svsinp_fcc
shdotc_fcc sptci_fcc
spvtas_fcc
vertc_fcc 0.25 sptp_fcc
sptcd_fcc
gsfmtvscmd_fcc
uvss_fcc
uvnvses_fcc
8
128
scmode
0.65
6000.0
-7900.0
deg_per_rad
738.0
sec_per_min 0.0
-1.0
spgamd_fcc
sphold
1
-1
0.0
spign_fcc
spnzlm_fcc
0.1
0.2
idle_arm_fcc
retard_fcc
spmode
ND
ND
ND
A B
A B
A B
1TAU*S+1
A B
1S
PFCModel
FunctionLibrary 2(4*184.5)
Honeywell
Boeing
pvsgmdpvscmdwmspd
pvsgn
vertspd209:22:24 08/29/1996Layer: 4
FIGURE 1.4.2-1 Vertical SpeedRef: D6-37704, Fig.2-29, Pg 2-67
*
*- LRU Only
IN
SYMMETRICAL LIMIT
Note: This page is only called when in either MCP orVNAV Vertical Speed modes (i.e., 128 is onlywritten into SCMODE in VNAV Vertical Speed.)
L
DD
N
IC
IC
IC
A
RS
TAU
H
L
N
N
D
A
A
B
B
BA
RSET
RSET
B
AL
SL
hold_fcc
svsinp_fcc
shdotc_fcc sptci_fcc
spvtas_fcc
vertc_fcc 0.25 sptp_fcc
sptcd_fcc
gsfmtvscmd_fcc
uvss_fcc
uvnvses_fcc
8
128
scmode
0.65
6000.0
-7900.0
deg_per_rad
738.0
sec_per_min 0.0
-1.0
spgamd_fcc
sphold
1
-1
0.0
spign_fcc
spnzlm_fcc
0.1
0.2
idle_arm_fcc
retard_fcc
spmode
ND
ND
ND
A B
A B
A B
1TAU*S+1
A B
1S
EngineModel
FunctionLibrary 1(4*184.5)
Honeywell
Boeing
pvsgmdpvscmdwmspd
pvsgn
vertspd209:22:24 08/29/1996Layer: 4
FIGURE 1.4.2-1 Vertical SpeedRef: D6-37704, Fig.2-29, Pg 2-67
*
*- LRU Only
IN
SYMMETRICAL LIMIT
Note: This page is only called when in either MCP orVNAV Vertical Speed modes (i.e., 128 is onlywritten into SCMODE in VNAV Vertical Speed.)
L
DD
N
IC
IC
IC
A
RS
TAU
H
L
N
N
D
A
A
B
B
BA
RSET
RSET
B
AL
SL
hold_fcc
svsinp_fcc
shdotc_fcc sptci_fcc
spvtas_fcc
vertc_fcc 0.25 sptp_fcc
sptcd_fcc
gsfmtvscmd_fcc
uvss_fcc
uvnvses_fcc
8
128
scmode
0.65
6000.0
-7900.0
deg_per_rad
738.0
sec_per_min 0.0
-1.0
spgamd_fcc
sphold
1
-1
0.0
spign_fcc
spnzlm_fcc
0.1
0.2
idle_arm_fcc
retard_fcc
spmode
ND
ND
ND
A B
A B
A B
1TAU*S+1
A B
1S
LRUSupplier
FunctionLibrary 3(4*184.5)
Honeywell
Boeing
pvsgmdpvscmdwmspd
pvsgn
vertspd209:22:24 08/29/1996Layer: 4
FIGURE 1.4.2-1 Vertical SpeedRef: D6-37704, Fig.2-29, Pg 2-67
*
*- LRU Only
IN
SYMMETRICAL LIMIT
Note: This page is only called when in either MCP orVNAV Vertical Speed modes (i.e., 128 is onlywritten into SCMODE in VNAV Vertical Speed.)
L
DD
N
IC
IC
IC
A
RS
TAU
H
L
N
N
D
A
A
B
B
BA
RSET
RSET
B
AL
SL
hold_fcc
svsinp_fcc
shdotc_fcc sptci_fcc
spvtas_fcc
vertc_fcc 0.25 sptp_fcc
sptcd_fcc
gsfmtvscmd_fcc
uvss_fcc
uvnvses_fcc
8
128
scmode
0.65
6000.0
-7900.0
deg_per_rad
738.0
sec_per_min 0.0
-1.0
spgamd_fcc
sphold
1
-1
0.0
spign_fcc
spnzlm_fcc
0.1
0.2
idle_arm_fcc
retard_fcc
spmode
ND
ND
ND
A B
A B
A B
1TAU*S+1
A B
1S
SimulatorManufacturer
FunctionLibrary 4
Current
(4*184.5)
Honeywell
Boeing
pvsgmdpvscmdwmspd
pvsgn
vertspd209:22:24 08/29/1996Layer: 4
FIGURE 1.4.2-1 Vertical SpeedRef: D6-37704, Fig.2-29, Pg 2-67
*
*- LRU Only
IN
SYMMETRICAL LIMIT
Note: This page is only called when in either MCP orVNAV Vertical Speed modes (i.e., 128 is onlywritten into SCMODE in VNAV Vertical Speed.)
L
DD
N
IC
IC
IC
A
RS
TAU
H
L
N
N
D
A
A
B
B
BA
RSET
RSET
B
AL
SL
hold_fcc
svsinp_fcc
shdotc_fcc sptci_fcc
spvtas_fcc
vertc_fcc 0.25 sptp_fcc
sptcd_fcc
gsfmtvscmd_fcc
uvss_fcc
uvnvses_fcc
8
128
scmode
0.65
6000.0
-7900.0
deg_per_rad
738.0
sec_per_min 0.0
-1.0
spgamd_fcc
sphold
1
-1
0.0
spign_fcc
spnzlm_fcc
0.1
0.2
idle_arm_fcc
retard_fcc
spmode
ND
ND
ND
A B
A B
A B
1TAU*S+1
A B
1S
EngineModel
(4*184.5)
Honeywell
Boeing
pvsgmdpvscmdwmspd
pvsgn
vertspd209:22:24 08/29/1996Layer: 4
FIGURE 1.4.2-1 Vertical SpeedRef: D6-37704, Fig.2-29, Pg 2-67
*
*- LRU Only
IN
SYMMETRICAL LIMIT
Note: This page is only called when in either MCP orVNAV Vertical Speed modes (i.e., 128 is onlywritten into SCMODE in VNAV Vertical Speed.)
L
DD
N
IC
IC
IC
A
RS
TAU
H
L
N
N
D
A
A
B
B
BA
RSET
RSET
B
AL
SL
hold_fcc
svsinp_fcc
shdotc_fcc sptci_fcc
spvtas_fcc
vertc_fcc 0.25 sptp_fcc
sptcd_fcc
gsfmtvscmd_fcc
uvss_fcc
uvnvses_fcc
8
128
scmode
0.65
6000.0
-7900.0
deg_per_rad
738.0
sec_per_min 0.0
-1.0
spgamd_fcc
sphold
1
-1
0.0
spign_fcc
spnzlm_fcc
0.1
0.2
idle_arm_fcc
retard_fcc
spmode
ND
ND
ND
A B
A B
A B
1TAU*S+1
A B
1S
PFCModel
(4*184.5)
Honeywell
Boeing
pvsgmdpvscmdwmspd
pvsgn
vertspd209:22:24 08/29/1996Layer: 4
FIGURE 1.4.2-1 Vertical SpeedRef: D6-37704, Fig.2-29, Pg 2-67
*
*- LRU Only
IN
SYMMETRICAL LIMIT
Note: This page is only called when in either MCP orVNAV Vertical Speed modes (i.e., 128 is onlywritten into SCMODE in VNAV Vertical Speed.)
L
DD
N
IC
IC
IC
A
RS
TAU
H
L
N
N
D
A
A
B
B
BA
RSET
RSET
B
AL
SL
hold_fcc
svsinp_fcc
shdotc_fcc sptci_fcc
spvtas_fcc
vertc_fcc 0.25 sptp_fcc
sptcd_fcc
gsfmtvscmd_fcc
uvss_fcc
uvnvses_fcc
8
128
scmode
0.65
6000.0
-7900.0
deg_per_rad
738.0
sec_per_min 0.0
-1.0
spgamd_fcc
sphold
1
-1
0.0
spign_fcc
spnzlm_fcc
0.1
0.2
idle_arm_fcc
retard_fcc
spmode
ND
ND
ND
A B
A B
A B
1TAU*S+1
A B
1S
LRUSupplier
(4*184.5)
Honeywell
Boeing
pvsgmdpvscmdwmspd
pvsgn
vertspd209:22:24 08/29/1996Layer: 4
FIGURE 1.4.2-1 Vertical SpeedRef: D6-37704, Fig.2-29, Pg 2-67
*
*- LRU Only
IN
SYMMETRICAL LIMIT
Note: This page is only called when in either MCP orVNAV Vertical Speed modes (i.e., 128 is onlywritten into SCMODE in VNAV Vertical Speed.)
L
DD
N
IC
IC
IC
A
RS
TAU
H
L
N
N
D
A
A
B
B
BA
RSET
RSET
B
AL
SL
hold_fcc
svsinp_fcc
shdotc_fcc sptci_fcc
spvtas_fcc
vertc_fcc 0.25 sptp_fcc
sptcd_fcc
gsfmtvscmd_fcc
uvss_fcc
uvnvses_fcc
8
128
scmode
0.65
6000.0
-7900.0
deg_per_rad
738.0
sec_per_min 0.0
-1.0
spgamd_fcc
sphold
1
-1
0.0
spign_fcc
spnzlm_fcc
0.1
0.2
idle_arm_fcc
retard_fcc
spmode
ND
ND
ND
A B
A B
A B
1TAU*S+1
A B
1S
SimulatorManufacturer
Proposed
FunctionLibrary
![Page 13: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/13.jpg)
13
What is a Low Level Function?What is a Low Level Function?
![Page 14: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/14.jpg)
14
Example Implementation in GSDSExample Implementation in GSDS
![Page 15: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/15.jpg)
15
EASY5 Test HarnessEASY5 Test Harness
![Page 16: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/16.jpg)
16
Function AnalysisFunction Analysis
![Page 17: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/17.jpg)
17
Function SimulationFunction Simulation
![Page 18: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/18.jpg)
18
Discussion TopicsDiscussion Topics
Boeing Commercial Airplane Group simulations
– A bit of background to our work
GSDS & Auto Code Generation in simulation development
– A brief overview of GSDS and how auto code generation is applied
Easy5/GSDS Integration
– What problem are we solving?
Low Level Functions Project
– A first application
Conclusion
– Some final words
![Page 19: Integration of EASY5/GSDS for Auto Code Generation and Testing Mike Bingle, Associate Technical Fellow Model Based Processes and Tools Simulation Engineering.](https://reader035.fdocuments.net/reader035/viewer/2022062619/5516b0b3550346f6208b5239/html5/thumbnails/19.jpg)
19
ConclusionConclusion
The Boeing Commercial Airplane Simulation Engineering group has
successfully integrated EASY5 and GSDS and applied the integrated
product in a production environment
...which leaves us well-positioned for the future