Global inverse optimal control of vertical take-off and landing aircraft

被引：1
|
作者：
Do, K. D. [1 ]
机构：
[1] Curtin Univ, Sch Civil & Mech Engn, Kent St, Bentley, WA 6102, Australia
来源：
IFAC JOURNAL OF SYSTEMS AND CONTROL | 2021年 / 15卷
关键词：
Vertical take-off and landing aircraft; Inverse optimality; K-infinity-exponential stability; TRACKING CONTROL; NONLINEAR CONTROL; OUTPUT TRACKING; PVTOL AIRCRAFT; VTOL AIRCRAFT; SYSTEMS; STABILIZATION;
D O I：
10.1016/j.ifacsc.2020.100132
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper formulates and solves a new problem of global practical inverse optimal control of underactuated vertical take-off and landing (VTOL) aircraft. The control design is based on a recent development of inverse optimal control design for nonlinear systems, and ensures global practical K-infinity-exponential stability of stabilization errors. More importantly, it also minimizes a cost function that penalizes both stabilization errors and control inputs without having to solve a Hamilton-Jacobi-Bellman or Hamilton-Jacobi-Isaacs equation. (C) 2020 Elsevier Ltd. All rights reserved.
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页数：10
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