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Volumn 27, Issue 1, 2004, Pages 118-126

Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; ATMOSPHERICS; COMPUTATIONAL GEOMETRY; COMPUTER SIMULATION; COMPUTER SOFTWARE; DEGREES OF FREEDOM (MECHANICS); FEEDBACK CONTROL; KINETIC THEORY; SPEED; THERMAL PLUMES;

EID: 1042286919     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.9336     Document Type: Article
Times cited : (209)

References (23)
  • 2
    • 85039572100 scopus 로고
    • Smithsonian Inst. Press, Washington, DC
    • Wolko, H. S. (ed.), The Wright Flyer, Smithsonian Inst. Press, Washington, DC, 1987, p. 48.
    • (1987) The Wright Flyer , pp. 48
    • Wolko, H.S.1
  • 4
    • 4243152080 scopus 로고
    • A Moving-Mass Roll Control System for a Fixed-Trim Reentry Vehicle
    • Jan.
    • Petsopoulos, T., and Regan, F. J., "A Moving-Mass Roll Control System for a Fixed-Trim Reentry Vehicle," AIAA Paper 94-0033, Jan. 1994.
    • (1994) AIAA Paper , vol.94 , Issue.33
    • Petsopoulos, T.1    Regan, F.J.2
  • 5
    • 24444442313 scopus 로고    scopus 로고
    • Considerations on the Design of Kinetic Kill Interceptor with Moving Mass Control
    • Dahlgren, VA, Aug.
    • Chadwick, W. R., and Malyevac, D. S., "Considerations on the Design of Kinetic Kill Interceptor with Moving Mass Control," Naval Surface Warfare Center, Rept. NSWCDD TR-00/87, Dahlgren, VA, Aug. 2000.
    • (2000) Naval Surface Warfare Center, Rept. , vol.NSWCDD TR-00-87
    • Chadwick, W.R.1    Malyevac, D.S.2
  • 7
    • 1042305023 scopus 로고    scopus 로고
    • Integrated Guidance-Control Systems for Fixed-Aim Warhead Missiles
    • AIAA, Reston, VA
    • Menon, P. K., and Ohlmeyer, E. J., "Integrated Guidance-Control Systems for Fixed-Aim Warhead Missiles," AIAA Missile Sciences Conf., AIAA, Reston, VA, 2000.
    • (2000) AIAA Missile Sciences Conf.
    • Menon, P.K.1    Ohlmeyer, E.J.2
  • 9
    • 84940905071 scopus 로고    scopus 로고
    • Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method
    • AIAA, Reston, VA
    • Mracek, C. P., and Cloutier, J. R., "Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method," Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA, Reston, VA, 1997, pp. 1697-1705.
    • (1997) Proceedings of the AIAA Guidance, Navigation and Control Conference , pp. 1697-1705
    • Mracek, C.P.1    Cloutier, J.R.2
  • 10
    • 0030678971 scopus 로고    scopus 로고
    • State-Dependent Riccati Equation Techniques: An Overview
    • American Automatic Control Council, Evanston, IL
    • Cloutier, J. R., "State-Dependent Riccati Equation Techniques: An Overview," Proceedings of the American Control Conference, American Automatic Control Council, Evanston, IL, 1997, pp. 932-936.
    • (1997) Proceedings of the American Control Conference , pp. 932-936
    • Cloutier, J.R.1
  • 12
    • 0003427480 scopus 로고
    • Prentice-Hall, Upper Saddle River, NJ
    • Marino, R., and Tomei, P., Nonlinear Control Design, Prentice-Hall, Upper Saddle River, NJ, 1995, pp. 41-60.
    • (1995) Nonlinear Control Design , pp. 41-60
    • Marino, R.1    Tomei, P.2
  • 14
    • 0024051348 scopus 로고
    • Flight Control Design Using Nonlinear Inverse Dynamics
    • Lane, S. H., and Stengel, R. F., "Flight Control Design Using Nonlinear Inverse Dynamics," Automatica, Vol. 24, No. 4, 1988, pp. 471-483.
    • (1988) Automatica , vol.24 , Issue.4 , pp. 471-483
    • Lane, S.H.1    Stengel, R.F.2
  • 15
    • 84867496030 scopus 로고
    • Application of Nonlinear Systems Inverses to Automatic Flight Control Design System Concepts and Flight Evaluation
    • edited by P. Kant, AGARDograph 251, July
    • Meyer, G., and Cicolani, L., "Application of Nonlinear Systems Inverses to Automatic Flight Control Design System Concepts and Flight Evaluation," Theory and Applications of Optimal Control in Aerospace Systems, edited by P. Kant, AGARDograph 251, July 1981.
    • (1981) Theory and Applications of Optimal Control in Aerospace Systems
    • Meyer, G.1    Cicolani, L.2
  • 16
    • 0035478988 scopus 로고    scopus 로고
    • Integrated Design of Agile Missile Guidance and Autopilot Systems
    • Aug.
    • Menon, P. K., and Ohlmeyer, E. J., "Integrated Design of Agile Missile Guidance and Autopilot Systems," IFAC Journal of Control Engineering Practice, Vol. 9, Aug. 2001, pp. 1095-1106.
    • (2001) IFAC Journal of Control Engineering Practice , vol.9 , pp. 1095-1106
    • Menon, P.K.1    Ohlmeyer, E.J.2
  • 20
    • 0242279727 scopus 로고    scopus 로고
    • The MathWorks, Inc., Natick, MA
    • Using Simulink®, The MathWorks, Inc., Natick, MA, 2000.
    • (2000) Using Simulink®
  • 22
    • 0033335428 scopus 로고    scopus 로고
    • Integrated Missile Guidance and Control: A State Dependent Riccati Differential Equation Approach
    • Inst. of Electrical and Electronics Engineers, Piscataway, NJ
    • 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, Inst. of Electrical and Electronics Engineers, Piscataway, NJ, 1999, pp. 243-248.
    • (1999) 1999 IEEE International Conference on Control Applications , pp. 243-248
    • Palumbo, N.F.1    Jackson, T.D.2
  • 23
    • 4243698768 scopus 로고    scopus 로고
    • Integrated Guidance-Autopilot Designs for Anti-Jam Operation of Precision Munitions
    • Optimal Synthesis Inc. Prepared Under Air Force Contract F08630-99-C-0040, Palo Alto, CA, Jan.
    • Menon, P. K., Dewell, L. D., and Sweriduk, G. D., "Integrated Guidance-Autopilot Designs for Anti-Jam Operation of Precision Munitions," Optimal Synthesis Inc., Final Rept. Prepared Under Air Force Contract F08630-99-C-0040, Palo Alto, CA, Jan. 2000.
    • (2000) Final Rept.
    • Menon, P.K.1    Dewell, L.D.2    Sweriduk, G.D.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.