ADAPTIVE BACKSTEPPING FLIGHT CONTROL WITH ACTUATOR SATURATION  

有作动器饱和的自适应多步回推飞行控制设计(英文)

作　　者：苏丙未[1] 陈欣[1] 曹云峰[1] 杨一栋[1] 

机构地区：[1]南京航空航天大学自动化学院

出　　处：《Transactions of Nanjing University of Aeronautics and Astronautics》2001年第1期81-85,共5页南京航空航天大学学报（英文版）

摘　　要：Because actuator satu ration can become a problem or even a disaster in flight control system, the con sideration of actuator saturation in the design phase may indeed reduce the degr ee of conservativeness of an flight control system (FCS) and thus noticeably enh ance the performance of the FCS. Deflection limits and rate limits are both cons idered in a new adaptive backstepping FCS design process. The key of the method is that a new control Lyapunov function (CLF) and a control law are chosen when the actuator saturation occurs. This idea results from that there must be a vari ation in the pseudo-control at saturation. The whole progress is a modification of an early presented method: adaptive backstepping control scheme. The stabili ty is proved and verified successfully. The conclusion and some comments about t his method are given in the end.由于作动器饱和会使飞控系统的性能恶化甚至引起飞行事故 ,所以在设计阶段考虑作动器饱和的影响可以减小飞控系统设计的保守性从而显著提高系统性能。在本文的自适应 BACKSTEPPING(回推 )飞控系统设计过程中考虑了作动器的位置和速率饱和。该方案的核心思想是在发生饱和的时候重新选取控制李雅普诺夫函数和自适应律。该思想是基于如下简单事实 :出现饱和时伪控制量将发生变化。整个设计过程是对早期提出的自适应回推控制方案的一个修正。该方案的稳定性得到了严格的数学证明和仿真验证。

关 键 词：nonlinear systems satu ration flight control system BACKSTEPPING adaptive control 

分 类 号：V241.4[航空宇航科学与技术—飞行器设计]