Model predictive control with wind preview for aircraft forced landing
Autonomous emergency landing capability of fixedwing aircraft is essential for opening airspace for civil unmanned aviation. This paper proposes a goal-oriented control scheme to exploit wind information for the benefit of forced landing. Different from general disturbances in a classic control system, a favorable wind would help aircraft to glide to a selected landing site more easily so increase the level of safety, while an adverse wind may render a selected landing site infeasible. We formulate the forced landing problem with wind preview information in the framework of Economic Model Predictive Control (EMPC) which aims to maximize the aircraft’s final altitude when reaching a target region.
A double-layer MPC scheme is adopted to lessen the computational burden and to increase the prediction time window for practical implementation, where a piecewise-constant disturbance preview based EMPC (DP-EMPC) maximizes the altitude at the upperlevel, and a linear MPC is employed at the lower-level to track the reference signal optimized by the upper-level planner. Moreover, the effectiveness of the goal-oriented optimal control scheme is illustrated by several case studies, where an unmanned aircraft is gliding towards potential landing sites under various conditions.
Funding
Goal-Oriented Control Systems (GOCS): Disturbance, Uncertainty and Constraints
Engineering and Physical Sciences Research Council
Find out more...National Natural Science Foundation of China (Grant Number: 62273165)
111 Project (Grant Number: B12018)
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Published in
IEEE Transactions on Aerospace and Electronic SystemsVolume
59Issue
4Pages
3995 - 4004Publisher
Institute of Electrical and Electronics Engineers (IEEE)Version
- AM (Accepted Manuscript)
Rights holder
© IEEEPublisher statement
© 2023 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.Acceptance date
2023-01-03Publication date
2023-01-09Copyright date
2023ISSN
0018-9251eISSN
1557-9603Publisher version
Language
- en