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。
The simulating results indicate that these flight path control laws can ensure the vehicle flies following the flight track of the towing plane.
计算结果表明，所采用的控制律可以实现运载器跟随拖曳飞机的飞行航迹。
Inverse problem of helicopter flight dynamics, to solve control laws from given motion, is important to the study for the maneuvering flight and the design for the advanced flight control system.
直升机飞行动力学逆问题是研究已知运动的控制规律，对直升机机动飞行和现代飞行控制律设计有重要意义。
The precondition of getting the systems performance is to solve the issue of flight path control laws of the towed vehicle in the system.
拖曳系统的飞行性能是评价拖曳系统可行性的一项基本内容，而要求解拖曳系统的飞行性能，则必须解决拖曳系统中运载器的航迹控制问题。
The precondition of getting the systems performance is to solve the issue of flight path control laws of the towed vehicle in the system.
拖曳系统的飞行性能是评价拖曳系统可行性的一项基本内容，而要求解拖曳系统的飞行性能，则必须解决拖曳系统中运载器的航迹控制问题。
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