Horizontal waypoint guidance design using optimal control

IEEE Transactions on Aerospace and Electronic Systems

Volumn 38, Issue 3, 2002, Pages 1116-1120

  Whang, Ick Ho ^a   Hwang, Tae Won ^a  

^a Agency for Defence Development   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; ASYMPTOTIC STABILITY; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; DIFFERENTIATION (CALCULUS); LAPLACE TRANSFORMS; LYAPUNOV METHODS; OPTIMAL CONTROL SYSTEMS;

HORIZONTAL WAYPOINT GUIDANCE ALGORITHM; LINEAR QUADRATIC REGULATOR; LYAPUNOV STABILITY THEOREM;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0036662722     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2002.1039430     Document Type: Letter

References (4)

1. Vian, J. L., and Moore, J. R. Trajectory optimization with risk minimization for military aircraft. Journal of Guidance, Control, and Dynamics, 12, 3, (May-June 1989), 311-317.
2. Rao, N. S., et al. (1990), Horizontal plane trajectory optimization for threat avoidance and waypoint rendezvous. In Proceedings of IEEE Aerospace and Electronics Conference, May 1990, 580-583.
3. Vaneck, T. W. (1997) Fuzzy guidance controller for an autonomous boat. IEEE Control Systems (Apr. 1997), 43-51.
4. Bryson, A. E., Jr., and Ho, Y. C. (1975) Applied Optimal Control. New York: Wiley, 1975.