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Volumn 23, Issue 4, 2000, Pages 742-746

Multiple model-based terminal guidance law

(1)  Rusnak, Ilan a  

a RAFAEL   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; COMPUTER SIMULATION; DISCRETE TIME CONTROL SYSTEMS; ESTIMATION; KALMAN FILTERING; LINEAR SYSTEMS; MATHEMATICAL MODELS; MISSILES; TIME VARYING CONTROL SYSTEMS; UNCERTAIN SYSTEMS;

EID: 0034226175     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4593     Document Type: Article
Times cited : (21)

References (11)
  • 3
    • 0026154544 scopus 로고
    • Optimal Guidance for High-Order and Acceleration Constrained Missile
    • Rusnak, I., and Levi, M., "Optimal Guidance for High-Order and Acceleration Constrained Missile," Journal of Guidance, Control, and Dynamics, Vol. 14, No. 3, 1991, pp. 589-596.
    • (1991) Journal of Guidance, Control, and Dynamics , vol.14 , Issue.3 , pp. 589-596
    • Rusnak, I.1    Levi, M.2
  • 4
    • 0026254981 scopus 로고
    • Discrete Optimal Guidance for High-Order Missile and Maneuvering Target
    • Nov.
    • Rusnak, I., "Discrete Optimal Guidance for High-Order Missile and Maneuvering Target," IEEE Transactions on Aerospace and Electronic Systems, Vol. 27, No. 6, Nov. 1991, pp. 870-872.
    • (1991) IEEE Transactions on Aerospace and Electronic Systems , vol.27 , Issue.6 , pp. 870-872
    • Rusnak, I.1
  • 5
    • 0023847080 scopus 로고
    • Can a Mixed Guidance Strategy Improve Missile Performance?
    • Forte, I., and Shinar, J., "Can a Mixed Guidance Strategy Improve Missile Performance?" Journal of Guidance, Control, and Dynamics, Vol. 11, No. 1, 1988, pp. 53-59.
    • (1988) Journal of Guidance, Control, and Dynamics , vol.11 , Issue.1 , pp. 53-59
    • Forte, I.1    Shinar, J.2
  • 6
    • 0024731525 scopus 로고
    • Improved Guidance Law Design Based on the Mixed-Strategy Concept
    • Forte, I., and Shinar, J., "Improved Guidance Law Design Based on the Mixed-Strategy Concept," Journal of Guidance, Control, and Dynamics, Vol. 12, No. 5, 1989, pp. 739-745.
    • (1989) Journal of Guidance, Control, and Dynamics , vol.12 , Issue.5 , pp. 739-745
    • Forte, I.1    Shinar, J.2
  • 7
    • 0005411134 scopus 로고    scopus 로고
    • Progress in Astronautics and Aeronautics, AIAA, Washington, DC, Chap. 5
    • Ben-Asher, J., and Yaesh, I., Advances in Missile Guidance Theory, Vol. 180, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1998, Chap. 5.
    • (1998) Advances in Missile Guidance Theory , vol.180
    • Ben-Asher, J.1    Yaesh, I.2
  • 8
    • 0015556075 scopus 로고
    • Adaptive Control of Linear Stochastic Systems
    • Deshpande, J. G., Upadhay, T. N., and Lainiotis, D. G., "Adaptive Control of Linear Stochastic Systems," Automatica, Vol. 9, 1973, pp. 107-115.
    • (1973) Automatica , vol.9 , pp. 107-115
    • Deshpande, J.G.1    Upadhay, T.N.2    Lainiotis, D.G.3
  • 11
    • 0026151633 scopus 로고
    • Reconfigurable Flight Control via Multiple Model Adaptive Control Methods
    • May
    • Maybeck, P. S., and Stevens, R. D., "Reconfigurable Flight Control via Multiple Model Adaptive Control Methods," IEEE Transactions on Aerospace and Electronic Systems, Vol. 27, No. 4, May 1991, pp. 470-480.
    • (1991) IEEE Transactions on Aerospace and Electronic Systems , vol.27 , Issue.4 , pp. 470-480
    • Maybeck, P.S.1    Stevens, R.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.