The Analysis of Miss Distance Sensitivity to Target Maneuvers for the Terminal Guidance System

Yu Yao; Xing Dan Wang; Bao Qing Yang; Jian Guo

doi:10.4028/www.scientific.net/AMM.128-129.710

Paper Titles

Research on High Precision and Non-Contact Measuring System for Geometric Parameter of the Irregular Shape
p.694

Research on Note Location of Wireless Sensor Network in Logistics Transportation
p.698

Research on Operational Model of New-Generation GPS Based on Dynamic Description Logic
p.702

Research on Temperature Monitoring System for Electrical Equipment Based on Wireless Sensor Networks
p.706

The Analysis of Miss Distance Sensitivity to Target Maneuvers for the Terminal Guidance System
p.710

The Application of Multiple Attribute Decision Making on Radio Signal Searching
p.714

The Detection of Soil Parameters by Portable near Infrared Spectrometer
p.718

The Route Algorithm of Post-Disaster Road Monitoring System
p.727

The Safety Monitoring of Colliery Equipments Based on Data Mining Technology
p.731

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 128-129The Analysis of Miss Distance Sensitivity to...

The Analysis of Miss Distance Sensitivity to Target Maneuvers for the Terminal Guidance System

Abstract:

This paper gives a new definition, the Miss Distance Sensitivity to Target Maneuvers (MDSTM), which evaluates the robustness of the Terminal Guidance System (TGS) and gives the degree of exact miss distance caused by the inaccurate estimates of target maneuver. In this paper, the criterion of sensitivity analysis is the ratio of miss distance to target maneuver. The form of the TPN is investigated and then the GTPN guidance law is also proposed. Then, considering cases that the flight control system without dynamics and the dynamics characteristic can not be ignored, the MDSTM performance of TGS governed with TPN and GTPN for step acceleration target maneuvers are analyzed. Finally, the sensitivity analysis results of the system are listed in the paper, and the conclusions of how the effect the MDSTM were given in the end of the paper.

You might also be interested in these eBooks

Measuring Technology and Mechatronics Automation IV

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 128-129)

Pages:

710-713

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.128-129.710

Citation:

Cite this paper

Online since:

October 2011

Authors:

Yu Yao, Xing Dan Wang, Bao Qing Yang, Jian Guo

Keywords:

Guidance Law, Sensitivity, Terminal Guidance System

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] YAO Y, JI Deng-gao, MA Ke-mao. General Design Trade-offs for a Precise Terminal Guidance System [J]. Infrared and Laser Engineering, Jun. 2008, Vol. 37(3): 382-385.

Google Scholar

[2] P. Zarchan. Tactical and Strategic Missile Guidance[M]. 5thed. American Institute of Aeronautics and Astronautics, (2007).

Google Scholar

[3] Khargonekar P P, Nagpal K M, Poolla K R. Control with Transients. SIAM J. Control and Optimization, 1991, 29(6): 1373-1393.

DOI: 10.1137/0329070

Google Scholar

[4] G. Siouris. Missile Guidance and Control Systems[M]. Springer, (2004).

Google Scholar

[5] Shukla U S, Mahapatra P R. The Proportional Navigation Dilemma - Pure or True[J] IEEE Transactions on AES, 1990, 26(2): 382-392.

DOI: 10.1109/7.53445

Google Scholar

[6] Richard V. Lawrence. Interceptor Line-of-Sight Rate Steering: Necessary Conditions for a Direct Hit[J]. Journal of Guidance, Control, and Dynamics. May-June 1998, Vol. 21(3): 471-476.

DOI: 10.2514/2.4260

Google Scholar

[7] JI Deng-gao. Performance Analysis via Finite-time Norm for Terminal Guidance[D]. Harbin: Harbin Institute of Technology. 2008, 12.

Google Scholar

[8] C. Kenney and R. Leipnik, Numerical integration of the differential matrix riccati equation, IEEE Transactions on Automatic Control, 1985, vol. 30(10): 962–970.

DOI: 10.1109/tac.1985.1103822

Google Scholar