阅读说明：本技术 自主无人航空机及其控制方法 (Autonomous unmanned aerial vehicle and control method thereof ) 是由 G·L·凯利 于 2018-12-18 设计创作，主要内容包括：一种自主无人航空机(10),包括机身、安装至所述机身的至少一个飞行系统(12)、适于控制所述或每个飞行系统的机载飞行控制器(18)、具有机器可读飞行控制指令的存储器存储单元、机载反馈系统,以及外部反馈系统,所述指令可由所述机载飞行控制器实施,所述机载反馈系统与所述飞行系统或每个飞行系统通信联接以向所述机载飞行控制器(18)提供实时内部飞行特性数据(18),其中,所述机载飞行控制器(18)被布置成从外部来源接收任务参数数据、根据所述任务参数数据确定起飞前飞行计划,并基于所述实时内部飞行特性数据和实时外部飞行特性数据来动态实施所述机器可读飞行控制指令以适应所述起飞前飞行计划而控制所述或每个飞行系统。(An autonomous unmanned aerial vehicle (10) comprising a fuselage, at least one flight system (12) mounted to the fuselage, an on-board flight controller (18) adapted to control the or each flight system, a memory storage unit having machine-readable flight control instructions, an on-board feedback system, and an external feedback system, the instructions being implementable by the on-board flight controller, the on-board feedback system being communicatively coupled with the or each flight system to provide real-time internal flight characteristic data (18) to the on-board flight controller (18), wherein the on-board flight controller (18) is arranged to receive mission parameter data from an external source, determine a pre-takeoff flight plan from the mission parameter data, and dynamically implement the machine-readable flight control instructions based on the real-time internal flight characteristic data and real-time external flight characteristic data to adapt the pre-takeoff flight plan to control the or each flight system A flight system.)