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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。
Describes the related specifications of the rate control / heading keeping (RCDH) response type in ADS-33E, simulates and analyzes the realization of heading rate command type, and proposes a test flight method of helicopter RCDH response type verification. It has been successfully applied to a RCDH response type verification flight test of a helicopter of helicopter type. The RCDH response type verification and the results of mid-range course change test and analysis under the type of response are given. The experimental results show that this method is suitable for the verification of the RCDH response type of helicopter.