Design and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim

In the digital simulation for the test and evaluation of the air-to-air missile, the problem of poor scalability and limited maneuver type of target aircraft model is outstanding. To resolve the above problem, the design and implementation of a six-degree-of-freedom target aircraft maneuvers simulat...

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Autor principal:	Guo Yajun, Ding Hua, Yang Dengtai, Zhou Xingdong
Formato:	article
Lenguaje:	ZH
Publicado:	Editorial Office of Aero Weaponry 2021
Materias:	\|target aircraft\|maneuver simulation model\|control law\|jsbsim\|test and evaluation Motor vehicles. Aeronautics. Astronautics TL1-4050
Acceso en línea:	https://doaj.org/article/ef1b2c0477b74c18a649bdf2d18f7e86
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id	oai:doaj.org-article:ef1b2c0477b74c18a649bdf2d18f7e86
record_format	dspace
spelling	oai:doaj.org-article:ef1b2c0477b74c18a649bdf2d18f7e862021-11-30T00:13:41ZDesign and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim1673-504810.12132/ISSN.1673-5048.2020.0222https://doaj.org/article/ef1b2c0477b74c18a649bdf2d18f7e862021-06-01T00:00:00Zhttps://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/1628469477810-1745440682.pdfhttps://doaj.org/toc/1673-5048In the digital simulation for the test and evaluation of the air-to-air missile, the problem of poor scalability and limited maneuver type of target aircraft model is outstanding. To resolve the above problem, the design and implementation of a six-degree-of-freedom target aircraft maneuvers simulation model is presented. Firstly, the control laws of normal overload, tangential overload and roll angle overload under different target maneuvers are designed. Then, the control models of elevator, aileron and throttle of target aircraft are designed. Finally, the implementation of target maneuver simulation model based on open source dynamic model framework of JSBSim is put forward. The target aircraft simulation model is applied to the digital simulation for the test and appraisal of an air-to-air missile, and the result shows that maneuver trajectories of target model are consistent with the expected maneuver type and parameters.Guo Yajun, Ding Hua, Yang Dengtai, Zhou XingdongEditorial Office of Aero Weaponryarticle\|target aircraft\|maneuver simulation model\|control law\|jsbsim\|test and evaluationMotor vehicles. Aeronautics. AstronauticsTL1-4050ZHHangkong bingqi, Vol 28, Iss 3, Pp 77-82 (2021)
institution	DOAJ
collection	DOAJ
language	ZH
topic	\|target aircraft\|maneuver simulation model\|control law\|jsbsim\|test and evaluation Motor vehicles. Aeronautics. Astronautics TL1-4050
spellingShingle	\|target aircraft\|maneuver simulation model\|control law\|jsbsim\|test and evaluation Motor vehicles. Aeronautics. Astronautics TL1-4050 Guo Yajun, Ding Hua, Yang Dengtai, Zhou Xingdong Design and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim
description	In the digital simulation for the test and evaluation of the air-to-air missile, the problem of poor scalability and limited maneuver type of target aircraft model is outstanding. To resolve the above problem, the design and implementation of a six-degree-of-freedom target aircraft maneuvers simulation model is presented. Firstly, the control laws of normal overload, tangential overload and roll angle overload under different target maneuvers are designed. Then, the control models of elevator, aileron and throttle of target aircraft are designed. Finally, the implementation of target maneuver simulation model based on open source dynamic model framework of JSBSim is put forward. The target aircraft simulation model is applied to the digital simulation for the test and appraisal of an air-to-air missile, and the result shows that maneuver trajectories of target model are consistent with the expected maneuver type and parameters.
format	article
author	Guo Yajun, Ding Hua, Yang Dengtai, Zhou Xingdong
author_facet	Guo Yajun, Ding Hua, Yang Dengtai, Zhou Xingdong
author_sort	Guo Yajun, Ding Hua, Yang Dengtai, Zhou Xingdong
title	Design and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim
title_short	Design and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim
title_full	Design and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim
title_fullStr	Design and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim
title_full_unstemmed	Design and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim
title_sort	design and implementation of general target aircraft maneuver simulation model based on jsbsim
publisher	Editorial Office of Aero Weaponry
publishDate	2021
url	https://doaj.org/article/ef1b2c0477b74c18a649bdf2d18f7e86
work_keys_str_mv	AT guoyajundinghuayangdengtaizhouxingdong designandimplementationofgeneraltargetaircraftmaneuversimulationmodelbasedonjsbsim
_version_	1718406898081857536

Design and Implementation of General Target Aircraft Maneuver Simulation Model Based on JSBSim

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