New Guidance Law and Autopilot Design for Launch Rockets
| Authors: | Cheng Chia-Hao, EE, National Taiwan University, Taiwan
Yeh Fu-Kuang, EE, National Taiwan University, Taiwan
Fu Li-Chen, EECS, National Taiwan University, Taiwan |
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| Topic: | 7.3 Aerospace |
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| Session: | Launcher and Missile Systems |
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| Keywords: | Guidance, Autopilot, Differential Geometry, Sliding Mode, Rockets |
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Abstract
In this paper, the decision parts of a launch rocket---guidancelaw (GL) and autopilot---are discussed. In the controller design,the differential geometry and sliding mode control are employed.In addition to the individual GL and autopilot system, stabilityof the integrated guidance/autopilot (G/A) system are discussed.Finally, various simulations are demonstrated to examine thefeasibility and performance of the rocket's integrated G/A system.
