Integrated guidance and control against ground fixed targets based on backstepping and input-to-state stability

Author

Weicheng, Ma ; Han, Yan ; Haibo, Ji

Author_Institution

Dept. of Autom., Univ. of Sci. & Technol. of China, Hefei, China

fYear

2012

fDate

5-8 Aug. 2012

Firstpage

321

Lastpage

326

Abstract

Based on the backstepping approach and input-tostate stability (ISS), an integrated guidance and control (IGC) algorithm for homing missiles against ground fixed targets is proposed in this paper. The model of the IGC system in the pitch plane is established, then the backstepping approach is adopted to design the IGC law so that the missile can hit the target with a desired impact attitude angle, and the stability of the overall system can be guaranteed as well although the model uncertainties exist. The numerical simulation results of the pursuit-evasion game show the effectiveness of the scheme.

Keywords

game theory; missile control; stability; uncertain systems; backstepping approach; ground fixed target; homing missile; input-to-state stability; input-tostate stability; integrated control; integrated guidance; model uncertainty; pitch plane; pursuit-evasion game; system stability; Aerodynamics; Backstepping; Missiles; Numerical models; Numerical stability; Stability criteria; Integrated guidance and control; backstepping; ground fixed target; input-to-state stability;

fLanguage

English

Publisher

ieee

Conference_Titel

Mechatronics and Automation (ICMA), 2012 International Conference on

Conference_Location

Chengdu

Print_ISBN

978-1-4673-1275-2

Type

conf

DOI

10.1109/ICMA.2012.6282862

Filename

6282862