单发螺旋桨飞机侧飞轨迹控制模型的仿真分析  

Simulation Analysis for Side Flight Trajectory Control of Single Propeller-driven Aircraft

作　　者：王艳红[1] 赵文智[1] 袁丁[1] 

机构地区：[1]中国民航大学飞行技术学院,天津300300

出　　处：《计算机仿真》2015年第6期26-30,共5页Computer Simulation

基　　金：中央高校基本科研业务费项目飞行专项(3122013X004)

摘　　要：研究单发螺旋桨飞机侧飞轨迹精确控制问题。在侧飞轨迹控制系统中,单发螺旋桨飞机侧飞过程较为复杂,单一的控制模式导致轨迹控制过程需要设定大量的约束条件。传统的飞机飞行轨迹控制模型为了满足约束条件,都是假设飞机独立控制信号的数目小于约束的自由度,将造成飞机的空间位置和姿态耦合,无法对飞机的空间位置和姿态进行独立控制,降低了侧飞轨迹控制能力。提出采用PD前馈控制算法的单发螺旋桨飞机侧飞轨迹控制方法。针对单发螺旋桨飞机侧飞过程进行动力学描述,将侧飞轨迹控制中的空间位置控制作为主要的控制对象。根据侧飞轨迹设计控制律,选取控制系统的位置和速度误差,设计轨迹控制的升力幅值的控制和力矩矢量的控制,实现单发螺旋桨飞机侧飞轨迹控制。实验结果表明,利用改进算法进行单发螺旋桨飞机侧飞轨迹控制,能够降低控制误差,满足单发螺旋桨飞机飞行需求。A side flight trajectory control method of single propeller driven aircraft based on PD feedforward con- trol algorithm was proposed in the paper. For the side flight process of single propeller driven aircraft, a dynamics de- scription was made. The spatial position control in the process of side flight trajectory control was taken as the main control objects. According to the control law of side flight trajectory design, the position and velocity error of control system were selected, and the control of lift force amplitude controlled by trajectory and torque vector were designed, to realize the side flight trajectory control of single propeller driven aircraft. The experimental results show that using the improved algorithm for the side flight trajectory control of single propeller - driven aircraft, can reduce the control error and meet the demand of single propeller - driven aircraft flight.

关 键 词：单发螺旋桨 侧飞轨迹 控制 

分 类 号：F127[经济管理—世界经济]