论文信息 - Attitude control of the landing demonstrator PHOENIX

Attitude control of the landing demonstrator PHOENIX

Phoenix is a national German un-powered landing demonstrator, which was designed as a precursor project within the frame of the next generation launcher program. A first in-flight demonstration has been successfully performed in May 2004 with three fully automated landings on a concrete landing strip at the NEAT test range in Sweden. The emphasis of this paper is on the attitude control of Phoenix. After a brief summary of the overall control structure, the paper describes in detail the design steps leading to the attitude control algorithm and presents flight data from the test

H. Strauch

[1] R. A. Hyde,et al. H [infinity] aerospace control design : a VSTOL flight application , 1995 .

[2] J. Doyle,et al. Essentials of Robust Control , 1997 .

[3] G. Vinnicombe. Uncertainty and Feedback: 8 loop-shaping and the-gap metric , 2000 .

[4] R. V. Jategaonkar,et al. Data Analysis of Phoenix RLV Demonstrator Flight Test , 2005 .

[5] G. Vinnicombe. Uncertainty and Feedback: H-[infinity] loop shaping and the v-gap metric , 2000 .

[6] Richard A. Hyde,et al. H Aerospace Control Design , 1996 .