Application of Maximum Principle with Final State Constraints in Gliding Control for Guided Bombs

Author

Geng, Lina ; Zheng, Zhiqiang

Author_Institution

Nat. Univ. of Defense Technol., Changsha

fYear

2007

fDate

18-21 Aug. 2007

Firstpage

205

Lastpage

209

Abstract

The optimal gliding control problem is studied for guided bombs. Optimal control theory is used to describe the characteristics of continuous variation in gliding control system for guided bombs. The optimal control model of guided bomb is built and solved using maximum principle with final state constraints and shooting method for boundary values. The shooting method is modified to meet desired performance index, final states and temporal constraints. An example for guided bomb optimal gliding is given to validate the effectiveness of proposed method.

Keywords

boundary-value problems; differential equations; maximum principle; military aircraft; missile guidance; aircraft bomb; boundary value shooting method; differential equation; final state constraint; guided bomb; maximum principle; optimal gliding control system; Aerodynamics; Automatic control; Automation; Dynamic programming; Educational institutions; Logistics; Mechatronics; Optimal control; Performance analysis; Weapons; costate vector; guided bomb; maximum principle; optimal control; shooting method for boundary value;

fLanguage

English

Publisher

ieee

Conference_Titel

Automation and Logistics, 2007 IEEE International Conference on

Conference_Location

Jinan

Print_ISBN

978-1-4244-1531-1

Type

conf

DOI

10.1109/ICAL.2007.4338557

Filename

4338557