A novel nonlinear adaptive control method is presented for a near-space hypersonic vehicle (NHV) in the presence of strong uncertainties and disturbances.
针对存在强烈不确定和干扰的近空间高超声速飞行器(NHV)，提出了一种新的非线性自适应控制方法。
The stability analyses of the NHV close-loop system are provided and it is proved that the system error and the weight learning error are uniformly ultimately hounded.
文中提供了NHV的闭环系统稳定性分析，经过证明系统误差和权值学习误差一致最终有界。
The stability analyses of the NHV close-loop system are provided and it is proved that the system error and the weight learning error are uniformly ultimately hounded.
文中提供了NHV的闭环系统稳定性分析，经过证明系统误差和权值学习误差一致最终有界。
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