TY - GEN
T1 - Model-based implementation of an onboard STANAG 4586 vehicle specific module for an air vehicle
AU - Hochstrasser, Markus
AU - Krause, Christoph
AU - Schneider, Volker
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2017
Y1 - 2017
N2 - This paper describes aspects of the system and model-based software design for a Vehicle Specific Module compliant to the NATO interoperability standard STANAG 4586 Edition 3 for Unmanned Air Vehicle Control Systems. The module enables controlling and monitoring of an air vehicle from a ground control station. It thereby serves as converter between custom interfaces of the controller on the one side, and an event-based communication based on data link messages described by the standard on the other side. The paper discusses important concepts of STANAG 4586 and outlines their adaption for the use in a manned research aircraft. Based on the system concept, the model-based software design in MATLAB Simulink/Stateflow is derived. Software details concerning a hybrid architecture merging auto-generated and conventionally programmed code as well as software interfaces are highlighted and presented in the context of modeling techniques for high-integrity systems.
AB - This paper describes aspects of the system and model-based software design for a Vehicle Specific Module compliant to the NATO interoperability standard STANAG 4586 Edition 3 for Unmanned Air Vehicle Control Systems. The module enables controlling and monitoring of an air vehicle from a ground control station. It thereby serves as converter between custom interfaces of the controller on the one side, and an event-based communication based on data link messages described by the standard on the other side. The paper discusses important concepts of STANAG 4586 and outlines their adaption for the use in a manned research aircraft. Based on the system concept, the model-based software design in MATLAB Simulink/Stateflow is derived. Software details concerning a hybrid architecture merging auto-generated and conventionally programmed code as well as software interfaces are highlighted and presented in the context of modeling techniques for high-integrity systems.
UR - http://www.scopus.com/inward/record.url?scp=85085847049&partnerID=8YFLogxK
U2 - 10.2514/6.2017-0809
DO - 10.2514/6.2017-0809
M3 - Conference contribution
AN - SCOPUS:85085847049
SN - 9781624104510
T3 - AIAA Modeling and Simulation Technologies Conference, 2017
BT - AIAA Modeling and Simulation Technologies Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Modeling and Simulation Technologies Conference, 2017
Y2 - 9 January 2017 through 13 January 2017
ER -