Robust flight control law design for an automatic landing flight experiment |
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| Affiliation: | 1. Mitsubishi Heavy Industries, LTD., Nagoya Aerospace Systems Works, 10 Oye-cho Minato-ku, Nagoya, 455-8515 Japan;2. National Aerospace Laboratory, 7-44-1 Jindaiji-higashimachi, Chofu-shi, Tokyo, 182-8522 Japan;3. National Space Development Agency of Japan, 2-4-1 Hamamastu-cho, Minato-ku, Tokyo, 105-8060 Japan;1. Department of Physics and Astronomy, University of Kentucky, Lexington, KY 40506-0055, USA;2. Department of Physics and Astronomy, Northwestern University, Evanston, IL 60208-3112, USA;3. Department of Electrical and Computer Engineering, University of Kentucky, Lexington, KY 40506-0055, USA;1. Shanghai Engineering Research Center of Ultra-Precision Optical Manufacturing, Fudan University, Shanghai 200438, PR China;2. School of Information Engineering, Guizhou Minzu University, Guiyang 550025, PR China |
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| Abstract: | The Automatic Landing FLight EXperiment, ALFLEX, was conducted by the National Aerospace Laboratory and National Space Development Agency of Japan, in order to develop their automatic landing technology for future unmanned reentry space vehicle. All the flight experiments were successfully completed. Because the ALFLEX vehicle is an unmanned and autonomous vehicle which has tip-fin wings, the flight control law has to achieve high-response-performance and robustness simultaneously. In this paper, the design method used to achieve these objectives is presented, as well as the results of flight experiments related to performance and robustness. |
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