Hostname: page-component-cd9895bd7-gbm5v Total loading time: 0 Render date: 2024-12-25T05:40:47.605Z Has data issue: false hasContentIssue false
  • English
  • Français

Observability-enhanced proportional navigation guidance with bearings-only measurements

Published online by Cambridge University Press:  17 February 2009

Mingyan Li  and
Cheng-Chew Lim
Mingyan Li
Affiliation:
Department of Electrical and Electronic Engineering, The University of Adelaide, SA 5005, Australia.
Cheng-Chew Lim
Affiliation:
Department of Electrical and Electronic Engineering, The University of Adelaide, SA 5005, Australia.
Rights & Permissions [Opens in a new window]

Abstract

Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.

We analyse the performance of the additive observable proportional navigation guidance system, which is well-suited for low-cost homing missiles with bearings-only measurements. Closed-form solutions are derived for both manoeuvring and non-manoeuvring targets. Guidelines on how to select the navigation constants of the control law are presented. We show that the additive observable proportional navigation guidance system can cover a larger capture area than can a conventional proportional navigation system.

Type
Research Article
Information
The ANZIAM Journal , Volume 40 , Issue 4 , April 1999 , pp. 497 - 512
Copyright
Copyright © Australian Mathematical Society 1999

References

[1 ]Hassoun, G. E., “Study of observability-enhanced guidance system”, Ph. D. Thesis, The University of Adelaide, October 1995.Google Scholar
[2]Hassoun, G. E. and Lim, C. C., “Advanced guidance control system design for homing missiles with bearings-only measurement”, in IEEE International Conference on Industrial Technology, (Guangzhou, China, December, 1994), 250–254.Google Scholar
[3]Hull, D. G., Speyer, J. L. and Burns, D. B., “Linear-quadratic guidance law for dual control of homing missiles”, J. of Guidance, Control and Dynamics 13 (1990) 137–144.CrossRefGoogle Scholar
[4]Murtaugh, S. A. and Criel, H. E., “Fundamentals of proportional navigation”, IEEE Spectrum December (1966) 75–85.CrossRefGoogle Scholar
[5]Patrick, H. L., Seltzer, S. M. and Warren, M. E., “Guidance laws for short-range tactical missiles”, J. of Guidance and Control 4 (1981) 98–108.CrossRefGoogle Scholar
[6]Speyer, J. L., Hull, D. G. and Bernard, W. P., “Performance of the modified-gain extended Kalman filter along an enhanced information path of a homing missile”, in Proceedings of the AIAA Guidance and Control Conference (Williamsburg, Virginia, August 1986), 48–56.Google Scholar
[7]Speyer, J. L., Hull, D. G. and Tseng, C. Y., “Estimation enhancement by trajectory modulation for homing missiles”, J. of Guidance, Control and Dynamics 7 (1984) 167–174.CrossRefGoogle Scholar
[8]van der Waerden, B. L., Mathematical Statistics (George Allen and Unwin Ltd., London, 1969).CrossRefGoogle Scholar
[9]Yang, C. D., Hsiao, H. B. and Yeh, F. B., “Generalized guidance law for homing missiles”, IEEE Transactions on Aerospace and Electronic Systems 25 (1989) 197–211.CrossRefGoogle Scholar
[10]Yang, C. D. and Yeh, F. B., “Closed-form solution for a class of guidance law”, J. of Guidance, Control and Dynamics 10 (1987) 412–415.CrossRefGoogle Scholar
[11]Yuan, P. J. and Chern, J. S., “Solutions of true proportional navigation for maneuvering and nonma-neuvering targets”, J. of Guidance, Control and Dynamics 15 (1992) 267–271.CrossRefGoogle Scholar