메뉴 건너뛰기




Volumn , Issue , 2003, Pages

Optimal fixed-interval integrated guidance-control laws for hit-to-kill missiles

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; CONTROL THEORY; ELECTRONIC GUIDANCE SYSTEMS; FLIGHT CONTROL SYSTEMS; STATE ESTIMATION;

EID: 85088722893     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5579     Document Type: Conference Paper
Times cited : (59)

References (17)
  • 1
    • 1042293326 scopus 로고    scopus 로고
    • Integrated Design of Agile Missile Guidance and Control System
    • November 17-19, Monterey, CA
    • Menon, P. K., Iragavarapu, V. R., and Ohlmeyer, E. J., "Integrated Design of Agile Missile Guidance and Control System", AIAA Missile Sciences Conference, November 17-19, 1998, Monterey, CA.
    • (1998) AIAA Missile Sciences Conference
    • Menon, P.K.1    Iragavarapu, V.R.2    Ohlmeyer, E.J.3
  • 2
    • 0033335428 scopus 로고    scopus 로고
    • Integrated Missile Guidance and Control: A State Dependent Riccati Differential Equation Approach
    • August 22-27, Kohala Coast, Hawai'i
    • Palumbo, N. F., and Jackson, T. D., "Integrated Missile Guidance and Control: A State Dependent Riccati Differential Equation Approach", 1999 IEEE International Conference on Control Applications, August 22-27, Kohala Coast, Hawai'i.
    • 1999 IEEE International Conference On Control Applications
    • Palumbo, N.F.1    Jackson, T.D.2
  • 3
    • 1042305023 scopus 로고    scopus 로고
    • Integrated Guidance-Control Systems for Fixed-Aim Warhead Missiles
    • November 7-9, Monterey, CA
    • Menon, P. K., and Ohlmeyer, E. J., "Integrated Guidance-Control Systems for Fixed-Aim Warhead Missiles", AIAA Missile Sciences Conference, November 7-9, 2000, Monterey, CA.
    • (2000) AIAA Missile Sciences Conference
    • Menon, P.K.1    Ohlmeyer, E.J.2
  • 4
    • 0035478988 scopus 로고    scopus 로고
    • Integrated Design of Agile Missile Guidance and Autopilot Systems
    • Menon, P. K. and Ohlmeyer, E. J., "Integrated Design of Agile Missile Guidance and Autopilot Systems", Control Engineering Practice, Vol. 9, 2001, pp. 1095-1106.
    • (2001) Control Engineering Practice , vol.9 , pp. 1095-1106
    • Menon, P.K.1    Ohlmeyer, E.J.2
  • 7
    • 0030150977 scopus 로고    scopus 로고
    • Root-Mean-Square Miss Distance of Proportional Navigation Missile Against Sinusoidal Target
    • May-June
    • Ohlmeyer, E. J., "Root-Mean-Square Miss Distance of Proportional Navigation Missile Against Sinusoidal Target," Journal of Guidance, Control, and Dynamics, Vol. 19, May-June 1996, pp. 563-568.
    • (1996) Journal of Guidance, Control, and Dynamics , vol.19 , pp. 563-568
    • Ohlmeyer, E.J.1
  • 8
    • 0002556590 scopus 로고    scopus 로고
    • Tactical and Strategic Missile Guidance
    • American Institute of Aeronautics and Astronautics, Reston, VA
    • Zarchan, P., Tactical and Strategic Missile Guidance, Progress in Astronautics and Aeronautics, Vol. 176, American Institute of Aeronautics and Astronautics, Reston, VA, 1997.
    • (1997) Progress In Astronautics and Aeronautics , vol.176
    • Zarchan, P.1
  • 9
    • 84999006699 scopus 로고
    • The Stability of Proportional Navigation Systems
    • August 20 -22, Portland, OR
    • Guelman, M., "The Stability of Proportional Navigation Systems", AIAA Guidance, Navigation and Control Conference, August 20 -22, 1990, Portland, OR.
    • (1990) AIAA Guidance, Navigation and Control Conference
    • Guelman, M.1
  • 16
    • 0142217187 scopus 로고    scopus 로고
    • Control of Terminal Engagement Geometry Using Generalized Vector Explicit Guidance
    • June 4 -6, Denver, CO
    • Ohlmeyer, E. J., "Control of Terminal Engagement Geometry Using Generalized Vector Explicit Guidance", Proceedings of the 2003 American Control Conference, June 4 -6, Denver, CO.
    • Proceedings of the 2003 American Control Conference
    • Ohlmeyer, E.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.