摘要
无人机飞行控制与管理系统担负着飞行控制、飞行管理、任务设备管理和火力控制等重要使命,在无人机系统研制中至关重要。根据对无人机飞行控制与管理系统组成与功能分析,介绍了基于仿真测试仪的控制与管理计算机动态仿真与测试方法,重点阐述了故障注入与测试方法;进而提出了飞行控制与管理系统动态仿真测试环境的构建原则和动态测试方法,最后指出了无人机飞行控制与管理系统动态仿真测试的后续发展趋势。
The flight control and management system is crucial in the development of UAV, which is undertook important missions of flight control, flight management, equipment management and firepower control. A new technology of dynamic simulation and test for control an management computer, which is based on the simulation tester, is introduced based on the analysis of flight control and management system composition and function of UAV. A method of fault injection and tes- ting is expounded with emphasis. Then the structure principle of the dynamic simulation test environment and the method of dynamic test for flight control and management system are put forward. The direction of dynamic simulation for flight control and management system is indicated finally.
出处
《导航定位与授时》
2014年第1期69-74,共6页
Navigation Positioning and Timing
关键词
无人机
飞行控制与管理
动态仿真测试
仿真测试仪
故障注入
UAV
Flight control and management system
Dynamic simulation and test
Simulation tester
Fault injec-tion