论文部分内容阅读
有控飞行器为了产生一个适合导引规律的空间法向力,轴对称型的理想横向运动应是无静差的。本文通过力矩耦合与运动耦合建立了可控非线性横向运动模型,较全面的分析了两种非线性耦合和自动驾驶仪非线性的影响。提出了对飞行,气动和自动笃驶仪等参数进行多维搜索寻优,可以获得准无静差的优化横向运动,并给出了用单纯彤法寻优的算例。
Controlled aircraft in order to produce a law suitable for the guidance of the spatial normal force, the ideal axisymmetric transverse motion should be no static. In this paper, a controllable nonlinear transverse motion model is established by the coupling of moment and motion, and the influences of two nonlinear coupling and autopilot nonlinearities are comprehensively analyzed. A multi-dimensional search optimization of flight, aerodynamic and automatic tutoring devices is proposed to obtain the quasi-no-error optimal lateral motion. An example is given to find the optimal solution with the simple method.