Optimal Guidance Law Design for Interception of Ballistic Missiles during the Boost Phase

Wei Wen Zhou; Xiao Geng Liang

doi:10.4028/www.scientific.net/AMM.135-136.655

Paper Titles

MRCluster: Mining Constant Row Bicluster in Gene Expression Data
p.628

Multiresolution Non-Local Mean Filter for Infrared Dim and Small Target Background Suppression
p.637

Narrow-Band Interference Suppression in Transform Domain in Tracking and Data Relay Satellite System
p.643

Optimal Estimation for Multiple Packet Dropouts Systems with Colored Measurement Noise
p.649

Optimal Guidance Law Design for Interception of Ballistic Missiles during the Boost Phase
p.655

Optimization of Adaptive Co-Ordination Based on Interaction Prediction Approach
p.660

Parameter Identification and Harmonic Analysis for EV Induction Motor Drive Systems
p.667

Path Planning for Mobile Robot Based on ACA-GA
p.673

Performance Comparison of Neighborhood Based Broadcasting Methods in MANETs
p.678

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 135-136Optimal Guidance Law Design for Interception of...

Optimal Guidance Law Design for Interception of Ballistic Missiles during the Boost Phase

Abstract:

An optimal guidance law for interception of ballistic missile during the boost phase is presented in this paper. The kinematics characteristics of tactical missile during its boost phase are analyzed firstly. Then based on the kinematics given and assumption, the relative kinematics equations between target and missile are established. Optimal guidance law via LQ optimization is derived under the specified cost function. The time-to-go estimation method is also given in the paper. In the end of this paper, simulation is executed and the results validate that the deduced guidance law satisfy the direct hit index.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 135-136)

Pages:

655-659

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.135-136.655

Citation:

Cite this paper

Online since:

October 2011

Authors:

Wei Wen Zhou, Xiao Geng Liang

Keywords:

Boost-Phase Interception, LQ Optimization, Optimal Guidance Law, Time-to-Go Estimation

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] John A Lukacs IV, Oleg A Yakimenko. Trajectory-Shaping Guidance for Interception of Ballistic Missiles During the Boost Phase[J]. Journal of Guidance, Control, and Dynamics Vol. 31, No. 5, September–October(2008). pp.1524-1531.

DOI: 10.2514/1.32262

Google Scholar

[2] John A Lukacs IV, Oleg A Yakimenko. Trajectory-Shape-Varying Missile Guidance for Interception of Ballistic Missiles during the Boost Phase[C]. AIAA Guidance, Navigation and Control Conference and Exhibit 20 - 23 August 2007, Hilton Head, South Carolina. pp.1-21.

DOI: 10.2514/6.2007-6538

Google Scholar

[3] M Guelman, O M Golan. Minimum Energy Guidance for Boost Phase Ballistic Missile Interception[C]. Proceedings of the American Control Conference, Seattle, Washington June 1995：pp.4131-4135.

DOI: 10.1109/acc.1995.532709

Google Scholar

[4] ZHANG Hong-yue; WANG Qing. Optimal Control Theory and Application [M],. High Education Company. 2006, pp.68-90.

Google Scholar

[5] ZHOU Di, Modern Guidance Laws for Homing Missile [M], National Defense Industrial Publishing Company. 2002 pp.88-98.

Google Scholar