摘要
This article addresses the problem of energy-optimal waypoint-following guidance for an unmanned aerial vehicle, considering a general autopilot dynamics model. The proposed guidance law is derived as a solution of a linear-quadratic optimal control problem in conjunction with a linearized kinematics model. The algorithm developed integrates path planning and path following into a single step, and can be applied to a general waypoint-following mission. Theoretical analysis reveals that previously suggested optimal point-to-point guidance laws are special cases of the proposed approach. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.
源语言 | 英语 |
---|---|
文章编号 | 8917649 |
页(从-至) | 2701-2717 |
页数 | 17 |
期刊 | IEEE Transactions on Aerospace and Electronic Systems |
卷 | 56 |
期 | 4 |
DOI | |
出版状态 | 已出版 - 8月 2020 |
已对外发布 | 是 |