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Volumn 2, Issue , 2005, Pages 1328-1352

Direct intercept guidance using differential geometry concepts

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; KINEMATICS; LYAPUNOV METHODS; MISSILES; NAVIGATION; TARGETS;

EID: 29744435975     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-5969     Document Type: Conference Paper
Times cited : (22)

References (21)
  • 2
    • 29744461144 scopus 로고    scopus 로고
    • Foundations of modern missile guidance
    • D. J. Salmond. Foundations of Modern Missile Guidance. Journal of Defence Science, 1(2):171-180, 1996.
    • (1996) Journal of Defence Science , vol.1 , Issue.2 , pp. 171-180
    • Salmond, D.J.1
  • 5
    • 0018492188 scopus 로고
    • On optimal guidance for homing missiles
    • S. Gutman. On Optimal Guidance for Homing Missiles. AIAA Journal of Guidance and Control, 3(4):296-300, 1979.
    • (1979) AIAA Journal of Guidance and Control , vol.3 , Issue.4 , pp. 296-300
    • Gutman, S.1
  • 6
    • 0024752960 scopus 로고
    • Assessment of air-to-air missile guidance and control technology
    • J. R. Cloutier, J. H. Evers, and J. J. Feeley. Assessment of Air-To-Air Missile Guidance and Control Technology. IEEE Control Systems Magazine, 9(6):27-34, 1989.
    • (1989) IEEE Control Systems Magazine , vol.9 , Issue.6 , pp. 27-34
    • Cloutier, J.R.1    Evers, J.H.2    Feeley, J.J.3
  • 10
    • 0004169843 scopus 로고
    • Schaum's Outline Series. McGraw-Hill, New York
    • M. M. Lipschutz. Differential Geometry. Schaum's Outline Series. McGraw-Hill, New York, 1969.
    • (1969) Differential Geometry
    • Lipschutz, M.M.1
  • 12
    • 0000392493 scopus 로고
    • Missile guidance by three dimensional proportional navigation
    • F. P. Adler. Missile Guidance by Three Dimensional Proportional Navigation. Journal of Applied Physics, 27:500-507, 1956.
    • (1956) Journal of Applied Physics , vol.27 , pp. 500-507
    • Adler, F.P.1
  • 16
    • 0032028247 scopus 로고    scopus 로고
    • Geometric approach to three dimensional missile guidance problem
    • Y. C. Chiou and C. Y. Kuo. Geometric approach to three dimensional missile guidance problem. Journal of Guidance, Control, and Dynamics, 21(2):335-341, 1998.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.2 , pp. 335-341
    • Chiou, Y.C.1    Kuo, C.Y.2
  • 21
    • 8744246973 scopus 로고
    • A general explicit, optimizing guidance law for rocket-propellant spacecraft
    • Paper 64-638
    • G. W. Cherry. A general explicit, optimizing guidance law for rocket-propellant spacecraft. In AIAA/ION Astrodynamics, Guidance and Control Conference, 1964. Paper 64-638.
    • (1964) AIAA/ION Astrodynamics, Guidance and Control Conference
    • Cherry, G.W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.