메뉴 건너뛰기




Volumn 28, Issue 1, 2005, Pages 162-166

New approach to guidance law design

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION MEASUREMENT; ALGORITHMS; LYAPUNOV METHODS; MANEUVERABILITY; MISSILES; MONTE CARLO METHODS; NAVIGATION; VELOCITY MEASUREMENT;

EID: 12744279533     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.6154     Document Type: Article
Times cited : (40)

References (12)
  • 1
    • 0003834502 scopus 로고    scopus 로고
    • Progress in Astronautics and Aeronautics, AIAA, Reston, VA
    • Zarchan, P. (ed.), Tactical and Strategic Missile Guidance, Vol. 176, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 1997.
    • (1997) Tactical and Strategic Missile Guidance , vol.176
    • Zarchan, P.1
  • 4
    • 0028256779 scopus 로고
    • True proportional navigation with maneuvering target
    • Ghose, D., "True Proportional Navigation with Maneuvering Target," IEEE Transactions on Aerospace and Electronic System. Vol. 30, No. 1, 1994, pp. 229-237.
    • (1994) IEEE Transactions on Aerospace and Electronic System. , vol.30 , Issue.1 , pp. 229-237
    • Ghose, D.1
  • 6
    • 0035393352 scopus 로고    scopus 로고
    • Design of missile guidance law via variable structure control
    • Moon, J., Kim, K., and Kim, J., "Design of Missile Guidance Law via Variable Structure Control," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 4, 2001, pp. 659-664.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.4 , pp. 659-664
    • Moon, J.1    Kim, K.2    Kim, J.3
  • 7
    • 0026254807 scopus 로고
    • An approach to design on control systems with parametric-coordinate feedback
    • Yanushevsky, R. T., "An Approach to Design on Control Systems with Parametric-Coordinate Feedback," IEEE Transactions on Automatic Control, Vol. 36, No. 11, 1991, pp. 1293-1295.
    • (1991) IEEE Transactions on Automatic Control , vol.36 , Issue.11 , pp. 1293-1295
    • Yanushevsky, R.T.1
  • 8
    • 0005411134 scopus 로고    scopus 로고
    • edited by P. Zarchan, Progress in Astronautics and Aeronautics, AIAA, Reston, VA
    • Ben-Asher, J. Z., and Yaesh, I., Advances in Missile Guidance Theory, edited by P. Zarchan, Vol. 180, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 1998.
    • (1998) Advances in Missile Guidance Theory , vol.180
    • Ben-Asher, J.Z.1    Yaesh, I.2
  • 9
    • 0033870946 scopus 로고    scopus 로고
    • Receding horizon guidance laws with no information on the time-to-go
    • Kim, K. B., Kim, M. J., and Kwon, W. H., "Receding Horizon Guidance Laws with No Information on the Time-to-Go," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 2, 2000, pp. 193-199.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.2 , pp. 193-199
    • Kim, K.B.1    Kim, M.J.2    Kwon, W.H.3
  • 11
    • 0026925747 scopus 로고
    • A controller design for a class of nonlinear systems using the lyapunov-bellman approach
    • Yanushevsky, R. T., "A Controller Design for a Class of Nonlinear Systems Using the Lyapunov-Bellman Approach," Journal of Dynamic Systems, Measurement and Control, Vol. 114, No. 9, 1992, pp. 390-394.
    • (1992) Journal of Dynamic Systems, Measurement and Control , vol.114 , Issue.9 , pp. 390-394
    • Yanushevsky, R.T.1
  • 12
    • 85089110260 scopus 로고    scopus 로고
    • Improving the high altitude performance of tail-controlled endoatmospheric missiles
    • Aug.
    • Zarchan, P., Greenberg, E., and Alpert, J., "Improving the High Altitude Performance of Tail-Controlled Endoatmospheric Missiles," AIAA Paper 2002-4770, Aug. 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.4770
    • Zarchan, P.1    Greenberg, E.2    Alpert, J.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.