CAJ | 학술논문

无人机控制系统仿真是验证无人机控制策略、故障诊断和优化航线等的主要方式。针对某型无人机的研制需求，分析了无人机仿真系统的原理和仿真信息的传递机制，提出并设计了基于全机仿真的无人机飞行控制仿真平台，包括：仿真计算机系统、飞行控制系统、地面测控系统和视景模拟系统。并将此仿真平台应用于某型无人机飞行控制系统的全机仿真试验中，试验和测试结果表明：该仿真平台设计合理并满足飞行仿真要求，具有一定的工程应用价值。
무인궤공제계통방진시험증무인궤공제책략、고장진단화우화항선등적주요방식。침대모형무인궤적연제수구，분석료무인궤방진계통적원리화방진신식적전체궤제，제출병설계료기우전궤방진적무인궤비행공제방진평태，포괄：방진계산궤계통、비행공제계통、지면측공계통화시경모의계통。병장차방진평태응용우모형무인궤비행공제계통적전궤방진시험중，시험화측시결과표명：해방진평태설계합리병만족비행방진요구，구유일정적공정응용개치。
The control system simulation for UAV is the main way to verify its control strategy,fault diag-nosis and optimal route etc. In view of the development needs for a certain UAV,we analyzed the theory of simulation system and transmission mechanism of simulation information,and proposed and designed the flight control simulation platform based on the whole machine simulation,which including:computer simu-lation system,flight control system,the measurement and control system and visual simulation system. The simulation platform was applied to the whole machine simulation test for a certain UAV. The test results show that the design of the simulation platform is reasonable and satisfied with the requirements of flight simulation,and has further engineering applications value.