Modeling of aircraft's maneuver in a pilot-in-loop flight simulation system

Kong Xiang-Jun, Gao Zheng-Hong

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper describes the modeling of aircraft's maneuver to support pilot-in-loop flight simulation. The aircraft's maneuver is modeled on base of analyzing the kinematical features of aircraft in different flight modes, related with airborne sensor working state and load release. According to the kinematical features, the relation between aircraft's maneuver and airborne sensor's working state and load release path/envelope is modeled. Through the model, the Pilot Control Instructions (PCI) can be simulated. The model can reflect not only the kinematical features of an aircraft but also the relation between aircraft motion and airborne sensor's working state and load release in modern flight. Resulting from the model, the simulated PCI can satisfy a pilot's needs in the flight simulation. The model is estimated through pilot-in-loop interception flight simulation. The results indicate the rationality of the model. The model can also be used in other states of aircraft's pilot-in-loop simulation system.

源语言英语
主期刊名Collection of Technical Papers - 2007 AIAA InfoTech at Aerospace Conference
2272-2277
页数6
出版状态已出版 - 2007
活动2007 AIAA InfoTech at Aerospace Conference - Rohnert Park, CA, 美国
期限: 7 5月 200710 5月 2007

出版系列

姓名Collection of Technical Papers - 2007 AIAA InfoTech at Aerospace Conference
3

会议

会议2007 AIAA InfoTech at Aerospace Conference
国家/地区美国
Rohnert Park, CA
时期7/05/0710/05/07

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