摘要
提出了一种采用新型抑制函数的地形跟随控制技术,并以某电传操纵飞机为例,设计了航迹倾角(γ)控制律,同时通过地形跟随六自由度仿真计算,比较了不同抑制函数对地形跟随性能的影响。仿真结果表明,采用该新型抑制函数后,飞机的地形跟随飞行性能得到了大大提高。
A terrain following technology with a new stay function was introduced in this paper. One fly-by-wire aircraft was used as an example. At first, its climbing track angle (γ) control law was designed. Then a six-degree-of-freedom nonlinear simulation was performed with several kinds of stay function. And the result shows that the new stay function can greatly improve the quality of the TF(terrain following) flying.
出处
《飞行力学》
CSCD
北大核心
2007年第3期12-16,共5页
Flight Dynamics
关键词
地形跟随
适应角法
航迹倾角控制律
抑制函数
terrain following
adapt angle method
climbing track angle (γ) control law
stay function