大机动无人机飞行控制系统的设计与试验

本文着重介绍大机动无人机KJ-9C行控制系统的设计思想和所采取的技术措施,从而解决了如何稳定地进入和安全地退出大机动飞行,以及如何保持稳定盘旋等技术难题。通过方案选择、调节规律的确定、系统的组成、仿真技术的应用和机载鉴定试飞的全过程,证明这套控制系统既能满足无人机的战术要求,又易于工程实现。

Design and Test of the Control System of High Maneuver Pilotless Aircraft

This paper describes the design concept of flight control system of a remote pilotless vehicle. The main problem solved by the authors was how to steadily enter into and safely withdraw from a highly maneuvera--ble flight. Some methods for keeping a steady circular flight path are also discussed. The whole development project includes the arrangement of the control system, the ground simulation test and finally, the demonstration flight test on an RPV. The flight test results show that the KJ-9C flight control system meets the tactical and technical requirements of the RPV satisfactorily and can be realized easily in engineering practice.