The advanced aircraft has those technological characteristics: stealth, supersonic cruise, super maneuverability, multi-target attack, multi-role, high load, long range cruise, integrated avionics, short takeoffs and vertical landings. These characteristics need multisubsystem integration in the advanced aircraft. In order to meet the need of advance aircraft, the nonlinear control system is necessary. In this paper, the nonlinear structure adaptive model inversion system was first used for the nonlinear control problem of super-maneuver aircraft. The sufficient and necessary condition of the control law was analyzed. Finally the results of the height-angle maneuver simulation show that the designed control system has good performance.
|頁（從 - 到）||928-935|
|期刊||Journal of Robotics and Mechatronics|
|出版狀態||Published - 2016 十二月 1|
All Science Journal Classification (ASJC) codes
- Computer Science(all)
- Electrical and Electronic Engineering