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Volumn , Issue , 2002, Pages

Nonlinear target state estimation in homing guidance

Author keywords

[No Author keywords available]

Indexed keywords

ELECTRONIC GUIDANCE SYSTEMS; GUIDED MISSILES; NONLINEAR ANALYSIS; RANDOM PROCESSES; STOCHASTIC MODELS; STOCHASTIC SYSTEMS;

EID: 85087594629     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4772     Document Type: Conference Paper
Times cited : (6)

References (20)
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  • 4
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  • 5
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    • Talole, S.E.1    Banavar, R.N.2
  • 6
    • 0016034279 scopus 로고
    • Optimal Guidance with Maneuvering Targets
    • March
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  • 7
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    • An Adaptive Terminal Guidance Scheme Based on an Exponential Cost Criterion with Application to Homing Missile Guidance
    • June
    • Speyer, J. L., An Adaptive Terminal Guidance Scheme Based on an Exponential Cost Criterion with Application to Homing Missile Guidance, IEEE Transactions on Automatic Control, Vol. 26, No. 5, June 1976, pp. 371-375.
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    • Speyer, J.L.1
  • 10
    • 29744461144 scopus 로고    scopus 로고
    • Foundations of Modern Missile Guidance
    • April
    • Salmond, D. J., Foundations of Modern Missile Guidance, Journal of Defense Science, Vol. 1, No. 2, April 1996, pp. 171-179.
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    • Salmond, D.J.1
  • 11
    • 0024752960 scopus 로고
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    • Cloutier, J. R., Evers, J. H., and Feeley, J. J., An Assessment of Air-to-Air Missile Guidance and Control Technology, IEEE Control Systems Magazine, Vol. 9, 1989, pp. 27-34.
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  • 15
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  • 20
    • 0028546574 scopus 로고
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.