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Adaptive Constrained On-board Guidance Technology forPowered Glide Vehicle
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作者 Huang Rong Wei Changzhu +1 位作者 Liu Yanbin Lu Yuping 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2017年第2期125-133,共9页
To make full use of expanded maneuverability and increased range,adaptive constrained on-board guidance technology is the key capability for a glide vehicle with a double-pulse rocket engine,especially under the requi... To make full use of expanded maneuverability and increased range,adaptive constrained on-board guidance technology is the key capability for a glide vehicle with a double-pulse rocket engine,especially under the requirements of desired target changing and on-line reconfigurable control and guidance.Based on the rapid footprint analysis,whether the new target is within the current footprint area is firstly judged.If not,the rocket engine ignites by the logic obtained from the analysis of optimal flight range by the method of hp-adaptive Gauss pseudospectral method(hp-GPM).Then,an on-board trajectory generation method based on powered quasi-equilibrium glide condition(QEGC)and linear quadratic regulator(LQR)method is used to guide the vehicle to the new target.The effectiveness of the guidance method consisted of powered on-board trajectory generation,LQR trajectory tracking,footprint calculation,and ignition time determination is indicated by some simulation examples. 展开更多
关键词 adaptive constrained on-board guidance double-pulse rocket engine hp-adaptive Gauss pseudospectral method powered quasi-equilibrium glide condition linear quadratic regulator(LQR)trajectory tracking
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