clearance of flight control laws 飞行控制律评估
The most common systematic approach to the design of flight control laws is based on the linearization model of UAV in different operating points.
常规控制器设计方案是在飞行包线内,迭代选择多个典型工作点后,利用无人机线性模型来设计飞行控制律。
参考来源 - 无人机动态特性分析及工作点设计自动化技术研究·2,447,543篇论文数据，部分数据来源于NoteExpress
The objective of this paper is to design the reentry flight control laws for the Suborbital Reusable Launch Vehicle(SRLV) based on nonlinear dynamic-inversion.
基于非线性动态逆理论，设计了亚轨道可重复使用运载器（SRLV）的再入控制律。
A nonlinear PD controller is presented in this paper and is used in the design of the control laws for an automatic terrain following flight control system.
提出了一种非线性PD控制方法，并将其应用在自动地形跟随系统飞行控制律的设计中。
The simulating results indicate that these static control laws can ensure the vehicle's equilibrium as it flies following the flight track of the towing plane.
仿真计算表明，所采用的控制律可以满足运载器飞行轨迹跟随拖曳飞机飞行轨迹时的飞行平衡特性。
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