Integrated guidance and control for hypersonic vehicles in dive phase with multiple constraints
Authors:
- JianHua WangJWJianHua Wang
- LuHua LiuLLLuHua Liu
- Tun ZhaoTZTun Zhao
- GuoJian TangGTGuoJian Tang
- 1 June 2016
- journal article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 53, 103-115
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Diving guidance via feedback linearization and sliding mode controlAerospace Science and Technology, 2015
- Partial integrated missile guidance and control with state observerNonlinear Dynamics, 2014
- Optimal diving maneuver strategy considering guidance accuracy for hypersonic vehicleActa Astronautica, 2014
- An Integrated Approach to Hypersonic Entry Attitude ControlInternational Journal of Automation and Computing, 2014
- Flight control for a flexible air-breathing hypersonic vehicle based on quasi-continuous high-order sliding modeJournal of Systems Engineering and Electronics, 2013
- Nonlinear hierarchy-structured predictive control design for a generic hypersonic vehicleScience China Technological Sciences, 2013
- Adaptive block dynamic surface control for integrated missile guidance and autopilotChinese Journal of Aeronautics, 2013
- Quasi-equilibrium glide adaptive guidance for hypersonic vehiclesScience China Technological Sciences, 2012
- Integrated Adaptive Guidance and Control for Re-Entry Vehicles with Flight Test ResultsJournal of Guidance, Control, and Dynamics, 2004
- Integrated Guidance and Control of Moving-Mass Actuated Kinetic WarheadsJournal of Guidance, Control, and Dynamics, 2004