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Volumn 26, Issue 3, 2005, Pages 263-267

Large angle attitude reaction jet control for an air-to-air missile

Author keywords

Air to air missile; Large angle attitude control; Reaction jet control; Sliding mode control

Indexed keywords

APPLICATIONS; CONTROLLABILITY; DESIGN; JETS; KINEMATICS; LYAPUNOV METHODS; PERFORMANCE; ROBUSTNESS (CONTROL SYSTEMS); SLIDING MODE CONTROL;

EID: 21144438086     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (10)

References (10)
  • 1
    • 0032071047 scopus 로고    scopus 로고
    • A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering
    • Ajay T, Mario I. A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering [J]. IEEE Trans on Control Systems Technology, 1998, 6(3): 359-371.
    • (1998) IEEE Trans on Control Systems Technology , vol.6 , Issue.3 , pp. 359-371
    • Ajay, T.1    Mario, I.2
  • 2
    • 21144458763 scopus 로고
    • Simultaneous reaction jet and aerodynamic control of missile systems
    • AIAA-93-3739-CP
    • Mario I, Ajay T. Simultaneous reaction jet and aerodynamic control of missile systems[R]. AIAA-93-3739-CP, 1993.
    • (1993)
    • Mario, I.1    Ajay, T.2
  • 3
    • 29744437533 scopus 로고    scopus 로고
    • Neural-adaptive nonlinear autopilot design for an agile anti-air missile
    • AIAA-96-3914
    • McFarland M B, Calise A J. Neural-adaptive nonlinear autopilot design for an agile anti-air missile[R]. AIAA-96-3914, 1996.
    • (1996)
    • McFarland, M.B.1    Calise, A.J.2
  • 4
    • 3042677139 scopus 로고    scopus 로고
    • Adaptive techniques for multiple actuator blending
    • AIAA-98-4494
    • Menon P K, Iragavarapu V R. Adaptive techniques for multiple actuator blending[R]. AIAA-98-4494, 1998.
    • (1998)
    • Menon, P.K.1    Iragavarapu, V.R.2
  • 5
    • 5144234618 scopus 로고    scopus 로고
    • Optimal thrust vector control of tactical missiles
    • AIAA-97-3475
    • Taur D R, Chern J S. Optimal thrust vector control of tactical missiles[R]. AIAA-97-3475, 1997.
    • (1997)
    • Taur, D.R.1    Chern, J.S.2
  • 6
    • 5144227697 scopus 로고
    • An analysis of the vertical launch phase of a missile concept
    • AIAA-83-0569
    • Solis R E. An analysis of the vertical launch phase of a missile concept[R]. AIAA-83-0569, 1983.
    • (1983)
    • Solis, R.E.1
  • 7
    • 21144452365 scopus 로고    scopus 로고
    • The characteristics analysis and simulation for an agile missile's turn motion with stabilized attitude
    • Chinese source
    • Wang P, CHEN W C, Yin X L. The characteristics analysis and simulation for an agile missile's turn motion with stabilized attitude[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2003, 23(2): 100-102. (in Chinese)
    • (2003) Journal of Projectiles, Rockets, Missiles and Guidance , vol.23 , Issue.2 , pp. 100-102
    • Wang, P.1    Chen, W.C.2    Yin, X.L.3
  • 8
    • 0037912309 scopus 로고    scopus 로고
    • Beijing: Beijing University of Aeronautics and Astronautics Press, Chinese source
    • Zhan R W. The satellite orbit and attitude dynamics and control[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 1998. 293-296. (in Chinese)
    • (1998) The Satellite Orbit and Attitude Dynamics and Control , pp. 293-296
    • Zhan, R.W.1
  • 9
    • 0034825442 scopus 로고    scopus 로고
    • Three-axes missile autopilot design: From linear to nonlinear control strategies
    • Devaud E. Three-axes missile autopilot design: from linear to nonlinear control strategies [J]. Journal of Guidance, Control and Dynamics, 2001, 24(1): 64-71.
    • (2001) Journal of Guidance, Control and Dynamics , vol.24 , Issue.1 , pp. 64-71
    • Devaud, E.1
  • 10
    • 0034261779 scopus 로고    scopus 로고
    • Kernel matrix of quaternion and its application in spacecraft attitude control
    • Chinese source
    • Chen W C, Xiao Y L, Zhao L H, et al. Kernel matrix of quaternion and Its application in spacecraft attitude control [J]. Acta Aeronautica et Astronautica Sinica, 2000, 21(5): 389-392. (in Chinese)
    • (2000) Acta Aeronautica et Astronautica Sinica , vol.21 , Issue.5 , pp. 389-392
    • Chen, W.C.1    Xiao, Y.L.2    Zhao, L.H.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.