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Optimal Guidance for Reusable Launch Vehicle in Reentry Phase Based on Adaptive Dynamic Programming with Experience Reply
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  • Xueyun WANG,
  • Yifan CHEN,
  • Yefeng XU,
  • Jialin WANG,
  • Jialin ZHU
Xueyun WANG
Beihang University School of Instrumentation Science and Opto-electronics Engineering

Corresponding Author:[email protected]

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Yifan CHEN
Beihang University School of Instrumentation Science and Opto-electronics Engineering
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Yefeng XU
Zhejiang University
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Jialin WANG
China Academy of Launch Vehicle Technology
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Jialin ZHU
China Academy of Launch Vehicle Technology
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Abstract

In this paper, an optimal tracking guidance method for Reusable Launch Vehicles (RLV) in reentry phase is proposed based on improved Adaptive Dynamic Programming (ADP) with experience reply (ER). The trajectory-tracking problem is transformed into a nonlinear affine optimization problem and solved by an infinite horizon optimal control scheme. An actor-critic ADP with novel network weight tuning algorithms is developed. By introducing the experience replay technique, the persistence of the excitation requirement can be assessed while updating the critic neural network and therefore the generalization performance is improved for the ADP based controller. Through Lyapunov stability theory, it is proved that the proposed control scheme can guarantee all states of the RLV system to be uniformly ultimately bounded. Simulations of both simple analytical nonlinear system and RLV guidance system under model uncertainty are conducted. In both cases better performances in terms of smoothness and accuracy are achieved compared with noise expansion, demonstrating the effectiveness and advantages of the proposed method for the optimal trajectory-tracking guidance of RLV.
Submitted to International Journal of Robust and Nonlinear Control
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