Research on Attitude Damage-Mitigating control of Air-breathing Hypersonic Flight Vehicles Based on Prescribed Performance

Jianhua Li, Yi Shen, Yunxin Li, Xuxin Bao, Haiyang Zhao
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Abstract

In order to delay the damage accumulation of the Air-breathing Hypersonic Flight Vehicle when it performs tasks efficiently, this paper designs a prescribed performance attitude damage-mitigating controller to achieve the above purpose. Firstly, established the flight vehicle’s force model and the damage dynamics model. Secondly, the concept of induced angle of attack is introduced, and a longitudinal short-period attitude model of the flight vehicle is established considering elasticity. Then, a prescribed performance attitude damage-mitigating controller is designed. The simulation results show that, on the basis of considering elastic factors, the attitude damage-mitigating controller can effectively delay the damage accumulation during the flight of the Air-breathing Hypersonic Flight Vehicle, while ensuring the mission performance, which provides an important reference in the future for maintaining the balance between mission performance and damage accumulation of flight vehicle.
基于规定性能的吸气式高超声速飞行器姿态减损控制研究
为了延缓吸气式高超声速飞行器在高效执行任务时的损伤积累,本文设计了一种规定性能姿态减伤控制器来实现上述目的。首先,建立了飞行器的受力模型和损伤动力学模型。其次,引入诱导攻角的概念,建立了考虑弹性的飞行器纵向短周期姿态模型;然后,设计了一种规定性能姿态减损控制器。仿真结果表明,在考虑弹性因素的基础上,姿态减伤控制器能有效延缓吸气式高超声速飞行器飞行过程中的损伤累积,同时保证任务性能,为今后保持任务性能与飞行器损伤累积之间的平衡提供重要参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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