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Volumn 23, Issue 4, 2000, Pages 693-700

Design of nonsaturating guidance systems

Author keywords

[No Author keywords available]

Indexed keywords

CONSTRAINT THEORY; CONTROL NONLINEARITIES; CONTROL SYSTEM SYNTHESIS; KINEMATICS; MANEUVERABILITY; MATHEMATICAL MODELS; MISSILES; NAVIGATION; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; TIME DOMAIN ANALYSIS; TRANSFER FUNCTIONS;

EID: 0034227171     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4585     Document Type: Article
Times cited : (20)

References (19)
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  • 2
    • 85006901940 scopus 로고
    • Advanced Guidance Laws for Acceleration Constrained Missile, Randomly Maneuvering Target and Noisy Measurement
    • Inst. of Electrical and Electronics Engineers, New York
    • Rusnak, I., "Advanced Guidance Laws for Acceleration Constrained Missile, Randomly Maneuvering Target and Noisy Measurement," Transactions of the IEEE Regional Conference on Aerospace Control Systems, Inst. of Electrical and Electronics Engineers, New York, 1993, pp. 453-462.
    • (1993) Transactions of the IEEE Regional Conference on Aerospace Control Systems , pp. 453-462
    • Rusnak, I.1
  • 3
    • 0018492188 scopus 로고
    • On Optimal Guidance for Homing Missiles
    • Gutman, S., "On Optimal Guidance for Homing Missiles," Journal of Guidance and Control, Vol. 2, No. 4, 1979, pp. 296-300.
    • (1979) Journal of Guidance and Control , vol.2 , Issue.4 , pp. 296-300
    • Gutman, S.1
  • 4
    • 0003326132 scopus 로고    scopus 로고
    • Horwood, West Sussex, England, UK, Chap. 5
    • Shneydor, N., Missile Guidance and Pursuit, Horwood, West Sussex, England, UK, 1998, Chap. 5, pp. 101-124.
    • (1998) Missile Guidance and Pursuit , pp. 101-124
    • Shneydor, N.1
  • 5
    • 0003275174 scopus 로고
    • Progress in Astronautics and Aeronautics, AIAA, Washington, DC, Chap. 2
    • Zarchan, P., Tactical and Strategic Missile Guidance, Vol. 124, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1990, Chap. 2, pp. 17-35.
    • (1990) Tactical and Strategic Missile Guidance , vol.124 , pp. 17-35
    • Zarchan, P.1
  • 6
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    • Divergence Range of Homing Missiles
    • July
    • Shinar, J., "Divergence Range of Homing Missiles," Israel Journal of Technology, Vol. 14, July 1976, pp. 47-55.
    • (1976) Israel Journal of Technology , vol.14 , pp. 47-55
    • Shinar, J.1
  • 7
    • 0032207926 scopus 로고    scopus 로고
    • Finite Time Stability Approach to Proportional Navigation Systems Analysis
    • Gurfil, P., Jodorkovsky, M., and Guelman, M., "Finite Time Stability Approach to Proportional Navigation Systems Analysis," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 853-861.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.6 , pp. 853-861
    • Gurfil, P.1    Jodorkovsky, M.2    Guelman, M.3
  • 8
    • 0017522241 scopus 로고
    • Analysis of Optimal Evasive Maneuvers Based on a Linearized Two-Dimensional Kinematic Model
    • Shinar, J., and Steinberg, D., "Analysis of Optimal Evasive Maneuvers Based on a Linearized Two-Dimensional Kinematic Model," Journal of Aircraft, Vol. 14, No. 8, 1977, pp. 795-802.
    • (1977) Journal of Aircraft , vol.14 , Issue.8 , pp. 795-802
    • Shinar, J.1    Steinberg, D.2
  • 9
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    • Complete Statistical Analysis of Nonlinear Missile Guidance Systems-SLAM
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    • (1979) Journal of Guidance and Control , vol.2 , Issue.1 , pp. 71-78
    • Zarchan, P.1
  • 10
    • 84944814967 scopus 로고
    • Some Results on the Theory of Physical Systems Governed by Nonlinear Functional Equations
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    • Sandberg, I.W.1
  • 11
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    • On Input-Output Stability of Time-Varying Nonlinear Feedback Systems - Part II: Conditions Involving Circles in the Frequency Plane and Sector Nonlinearities
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  • 17
    • 0004099251 scopus 로고
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    • Slotine, J. J. E., and Li, W., Applied Nonlinear Control, Prentice-Hall, Upper Saddle River, NJ, 1991, Chap. 4, pp. 128-143.
    • (1991) Applied Nonlinear Control , pp. 128-143
    • Slotine, J.J.E.1    Li, W.2
  • 19
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    • A Frequency Domain Condition for the Stability of Feedback Systems Containing a Single Time-Varying Nonlinear Element
    • Sandberg, I. W., "A Frequency Domain Condition for the Stability of Feedback Systems Containing a Single Time-Varying Nonlinear Element," Bell Systems Technical Journal, Vol. 43, 1964, pp. 1601-1608.
    • (1964) Bell Systems Technical Journal , vol.43 , pp. 1601-1608
    • Sandberg, I.W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.