DocumentCode :
630953
Title :
Hypersonic glider guidance using Model Predictive Control
Author :
Baldwin, Morgan ; Kolmanovsky, Ilya
Author_Institution :
Space Vehicles Directorate, Air Force Res. Lab., Albuquerque, NM, USA
fYear :
2013
fDate :
17-19 June 2013
Firstpage :
5550
Lastpage :
5555
Abstract :
A Model Predictive Control (MPC) approach to hypersonic glider flight management is proposed. Given the capability of MPC to handle constraints, it is promising for application to a hypersonic glider with path constraints. With this approach, the glider navigates through defined way points while avoiding exclusion zones. The minimum-time formulation of MPC is employed. The glider´s capability to perform the maneuvers is demonstrated using simulations.
Keywords :
aircraft control; collision avoidance; military aircraft; missile guidance; predictive control; MPC; constraint handling; exclusion zone avoidance; hypersonic glider flight management; hypersonic glider guidance; minimum-time formulation; model predictive control; path constraints; Equations; Mathematical model; Predictive control; Robustness; Solid modeling; Trajectory; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2013
Conference_Location :
Washington, DC
ISSN :
0743-1619
Print_ISBN :
978-1-4799-0177-7
Type :
conf
DOI :
10.1109/ACC.2013.6580706
Filename :
6580706
Link To Document :
بازگشت