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论文类型：会议论文

发表时间：2012-08-13

收录刊物：EI、Scopus

摘要：The Common Aero Vehicle (CAV) is a hypersonic reentry weapon platform which was researched and developed by Boeing for USA FALCON program. Aiming at the reentry guidance problem of CAV under complicated path constraints and terminal conditions, a generation method of three-dimensional reentry reference trajectory is presented, and then a trajectory tracking controller is designed using linear quadratic regulator (LQR) theory. Lateral guidance is realized by using bank-reversal strategy of bank angle with the aid of the azimuth error corridor. Finally, the reentry guidance results for CAV are presented based on the above method. ? 2011 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.