The embodiment of the invention discloses an aircraft airborne control system, which is used for a manned aircraft remotely driven through a ground control station, and comprises a redundant flight control system provided with at least three flight control units, one of the at least three flight control units is set as a main control unit which can be dynamically switched in the flight process, and the other one is set as an auxiliary control unit which can be dynamically switched in the flight process. All the flight control units except the main control unit are set as standby control units which can be dynamically switched in the flight process; and the pan-tilt control unit is connected with the redundant flight control system and is used for controlling a pan-tilt to execute actions according to the flight control instruction output by the redundant flight control system. The embodiment of the invention further discloses a corresponding aircraft control system and an aircraft. According to the invention, the flight control system can be ensured to safely and efficiently realize main and standby switching, and the probability that all the main and standby flight control systems fail is effectively avoided.
本申请实施例公开一种航空器机载控制系统,用于通过地面控制站远程驾驶的载人航空器,包括:设置有至少三个飞行控制单元的冗余飞行控制系统,所述至少三个飞行控制单元中的一个在飞行过程中被设置为可动态切换的主控制单元,除该主控制单元之外的飞行控制单元在该飞行过程中均被设置为可动态切换的备用控制单元;云台控制单元,与所述冗余飞行控制系统相连,用于按照所述冗余飞行控制系统输出的飞行控制指令控制云台执行动作。本申请实施例还公开了相应的航空器控制系统和航空器。本申请可确保飞行控制系统能够安全高效地实现主备切换,有效避免出现主备飞行控制系统全部故障的概率。
Aircraft onboard control system, aircraft control system and aircraft
航空器机载控制系统、航空器控制系统和航空器
2022-12-30
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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