Constrained Integrated Guidance and Control Scheme for Strap-Down Hypersonic Flight Vehicles with Partial Measurement and Unmatched Uncertainties

This paper investigates the issue of integrated guidance and control (IGC) design for strap-down hypersonic flight vehicles with partial measurement information and unmatched uncertainties. A constrained IGC scheme is proposed by combining the barrier Lyapunov function-based backstepping methodology...

Full description

Bibliographic Details
Main Authors: Minzhou Dong, Xinkai Xu, Feng Xie
Format: Article
Language:English
Published: MDPI AG 2022-12-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/9/12/840

Similar Items