Aiming point guidance law for air-to-air missiles

International Journal of Systems Science

Volumn 29, Issue 2, 1998, Pages 95-102

  Tsao, Lu Ping ^a   Chou, Ching Lain ^b   Chen, Chuen Ming ^a   Chen, Chi Teh ^a  

^a NATIONAL DEFENSE UNIVERSITY   (Taiwan)

^b CHUNG SHAN INSTITUTE OF SCIENCE AND TECHNOLOGY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; ERROR ANALYSIS; MATHEMATICAL MODELS; MISSILES;

AIMING POINT GUIDANCE (APG) LAW; AIR TO AIR MISSILES;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0032003513     PISSN: 00207721     EISSN: 14645319     Source Type: Journal    
DOI: 10.1080/00207729808929501     Document Type: Article

References (8)

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2. Gregory, P. C., 1972, General consideration in guidance and control technology. Guidance and Control of Tactical Missiles, AGARD Lecture Series No. 52, pp. 2.1-2.14.
3. Kim, Y. S., 1985, A new guidance law for homing missiles. Journal of Guidance,8, 402-404.
4. Patrick, H. L., and Seltzer, S. M., 1979, Future US Army missile G&C system.AIAA 79-1974, pp. 404-412.
5. Patrick, H. L., Seltzer, S. M., and Warren, M. E., 1979, Guidance laws for short-range tactical missiles. AIAA 79-0059R. Journal of Guidance and Control, 4,98-108.
6. Powell, M. J. D., 1966, Minimization of functions of several variables. Numerical Analysis, an Introduction (Academic Press).
7. Riggs, T. L., 1972, Optimal control and estimation for terminal guidance of tactical missiles. AGARD-LS-52 Guidance and Control of Tactical Missiles, 23.1-23.11.
8. Wiseman, A. P., and Mitchell, J. R., 1983, New navigation and guidance laws for homing missiles. IEEE SOUTHEASTCON '83, Orlando, pp. 582-586.