摘要
描述了ADS-33E中速率控制/航向保持(RCDH)响应类型的相关规范要求,对航向速率指令类型的实现进行了仿真和分析,提出了电传直升机RCDH响应类型验证试飞方法,并将该方法成功应用于某型电传直升机RCDH响应类型验证试飞中,给出了RCDH响应类型验证以及该响应类型下悬停中等幅度航向变化试飞结果及分析。试验结果表明,该方法适用于电传直升机RCDH响应类型的验证。
The paper mainly described the relevant criterion requirements for Rate Command Heading Hold （RCDH） response types in the performance standards of ADS-33E, simulated and analyzed the realization of heading rate command type, presented a flight test method for RCDH response types validation, and successfully applied the method in the flight test of a certain type FBW helicopter. Finally, presented the results and the analysis of RCDH response type verification and the mid-term amplitude heading change in hover. The flight test results show that the method is suitable for the validation of the RCDH response type on a FBW helicopter.
出处
《航空科学技术》
2017年第7期7-11,共5页
Aeronautical Science & Technology
