Release Time:2019-03-11  Hits:

Indexed by: Conference Paper

Date of Publication: 2012-08-13

Included Journals: Scopus、EI

Abstract: 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.