摘要
针对传统飞行控制系统的局限性，提出小型无人机飞行修正变结构控制策略．在纵向轨迹控制系统中引入一饱和型变结构控制器，实现姿态角与高度的自主复合控制，解决了小型无人机超低空飞行触地问题，同时提高了系统的可靠性．
In view of limit situation of traditional flight control system, an tactics of flight correctional variable structure control is given. A saturated variable structure controller is adopted in the vertical trace control system, the UAV's hedgehopping is solved and reliability of the system is improved.
出处
《信息与控制》
CSCD
北大核心
1999年第6期471-474,共4页
Information and Control
关键词
无人机
飞行控制
变结构控制
unmanned air vehicle(UAV), flight control, variable structure control
