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MAV Waypoint Guidance with Arrival Angle and Time Scheduling Constraints

机译:具有到达角和时间调度约束的MAV航点制导

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This paper presents a proportional navigation based method to control the arrival time and approach angle at the waypoint for a miniature aerial vehicle (MAV). The two constraints are simultaneously satisfied by a closed-form solution for the navigation gain. A two stage methodology is used where the initial phase orients the MAV to a desired feasible geometry for the second phase. Simulations are carried for different MAV initial conditions, with autopilot dynamics, and arrival angle and time constraints. The work presents a simple and robust methodology for the multi-constraint problem.
机译:本文介绍了一种基于比例的导航方法,以控制微型航空车辆(MAV)航点的到达时间和接近角度。两个约束通过用于导航增益的闭合方案同时满足。使用两个阶段方法,其中初始阶段或者将MAV变为第二阶段的期望可行几何形状。使用自动驾驶仪动态和到达角度和时间约束来携带不同的MAV初始条件。该工作为多约束问题提供了一种简单且鲁棒的方法。

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