제어로봇시스템학회:학술대회논문집
- 제어로봇시스템학회 2001년도 ICCAS
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- Pages.148.5-148
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- 2001
An Adaptive Flight Control Law Design for the ALFLEX Flight Control System
- Imai, Kanta (Nihon Univ.) ;
- Shimada, Yuzo (Nihon Univ.) ;
- Uchiyama, Kenji (Nihon Univ.)
- 발행 : 2001.10.01
초록
In this report, an adaptive flight control law based on a linear-parameter-varying (LPV) model is presented for a flight control system. The control system is designed to track an output of a vehicle to a reference signal from the guidance system, which generates a reference flight path. The proposed adaptive control law adjusts the controller gains continuously on line as flight conditions change. The obtained adaptive controller guarantees global stability over a wide flight envelope. Computer simulation involving six-degree-of-freedom nonlinear flight dynamics is applied to Japan´s automatic landing flight experimental vehicle (ALFLEX) to examine the effectiveness of the proposed adaptive flight control law.
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