研究了空天飞行器（ASV）再入跨大气层飞行时的姿态控制问题。
The problems concerning an aerospace vehicle's(ASV) atmospheric reentry flight attitude control system were researched.
研究一种新的空天飞行器基于非线性干扰观测器的轨迹线性化飞行控制方案。
A novel nonlinear disturbance observer-enhanced trajectory linearization control (TLC) structure is applied to an aerospace vehicle (ASV).
因此适于多性能协同优化设计的理论成为空天飞行器概念设计成败的一个关键。
Thus, the theory of synergetic optimization aerospace vehicles is becoming a key problem in designing.
应用推荐