Dynamic inversion (DI) theory is known well as nonlinear control theory. DI theory can cancel the nonlinear dynamics and linearize the input and output maps. Therefore, closed loop analysis through flight trajectory becomes easier than other control systems, e.g. gain tuning method. When we use...
Control law design The incremental nonlinear dynamic inversion (INDI) control law design procedure is covered in this section. The autonomous landing can be performed by using the same procedure while applying aircraft control law. After it has been decoupled, the structure of the design control law...
1.Fuzzy sliding mode control approach to mass moment interception missile based ondynamic inversion;基于动态逆的质量矩拦截弹模糊滑模控制 2.Design of Overload Control System for Winged Missile Using Fuzzy Dynamic Inversion Based on Three Time-Scale Separation;基于三时标分离的模糊动态逆飞航导弹过载控制...
To remove the motion aberrations from the forward imaging, backward inversion imaging methods are very interesting. Wang et al. proposed an active optical flow method to remove the residual high-frequency motion aberration of the forward active imaging approaches24. However, the optical flow has low...
2.Thenonlinear dynamic inversionis adopted to design flight control law of the nonlinear control system based on the UAV.应用非线性动态逆方法,根据无人机本身具有明显不同时间尺度差异的动力学特性,结合奇异摄动理论将控制变量按照响应快慢分为4个回路进行了控制器的设计与仿真;设计推力矢量控制和气动控制相结合...
1dright) of the qubits, we find a population inversion in the second case, which implies T < 0. While temperature is usually restricted to be non-negative for an unbounded energy spectrum to secure convergence of the partition function, negative absolute temperatures have been experimentally ...
A dynamic inversion control method based on variable structure theory is presented according to the feature that hypersonic vehicle model is highly nonlinear,strong coupled and includes uncertain parameters. 针对高超音速飞机模型的高度非线性、强耦合、参数不确定等特点,提出了基于变结构理论的动态逆控制方法。
A dynamic inversion control method based on variable structure theory is presented according to the feature that hypersonic vehicle model is highly nonlinear,strong coupled and includes uncertain parameters. 针对高超音速飞机模型的高度非线性、强耦合、参数不确定等特点,提出了基于变结构理论的动态逆控制方法...
Design of control systems for missiles based on dynamic inversion and decentralized control; 基于动态逆和分散控制的导弹控制系统设计 更多例句>> 补充资料:动态改性硅胶色谱法 分子式:CAS号:性质:又称动态改性色谱。将含有一定浓度固定液的流动相连续流过装有硅胶载体的色谱柱,至固定液在流动相和载体间达到分布...
In order to provide satisfactory nonlinear decoupling ability and maintain good longitudinal stability,we apply nonlinear dynamic inversion control in designing the flight control system of the hypersonic vehicle. 该文应用非线性动态逆控制来设计高超音速飞行控制系统,以求为其提供满意的非线性解耦控制能力,维...