The invention discloses a control method of an aircraft, the aircraft and a computer readable storage medium, and the method comprises the steps that a first flight control system obtains the state of the aircraft, the health state of airborne equipment and flight parameters collected by a sensing unit; determining the first service quality of the first flight control system according to the aircraft state, the health state of the airborne equipment and the flight parameters; and acquiring second service quality of the second flight control system, and determining a control role undertaken by the first flight control system according to the first service quality and the second service quality, so that the first flight control system can execute a control function corresponding to the control role of the first flight control system. Wherein the first service quality of each flight control system is determined by the own flight control system, and the second service quality of each flight control system is determined by other flight control systems. And the control roles of the flight control systems can be switched according to the service quality, so that the flight control system on a normal control path can also control equipment or modules with faults on other control paths, and the reliability of the aircraft is improved.
本发明公开了飞行器的控制方法、飞行器及计算机可读存储介质,该方法包括:第一飞控系统通过获取传感单元采集的飞行器状态、机载设备的健康状态和飞行参数,根据飞行器状态、机载设备的健康状态和飞行参数确定第一飞控系统的第一服务质量;获取第二飞控系统的第二服务质量,根据第一服务质量和第二服务质量确定第一飞控系统所承担的控制角色,使得第一飞控系统能执行自身控制角色对应的控制功能。其中,每个飞控系统的第一服务质量由自身飞控系统确定,第二服务质量由其他飞控系统确定。且由于各个飞控系统的控制角色能根据服务质量进行切换,使得正常控制路径上的飞控系统也能管控其他控制路径上发生故障的设备或模块,提高飞行器的可靠性。
Aircraft control method, aircraft and computer readable storage medium
飞行器的控制方法、飞行器及计算机可读存储介质
2023-06-02
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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