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Publikováno v:
International Journal of Aeronautical and Space Sciences. 18:334-343
Publikováno v:
IEEE Transactions on Aerospace and Electronic Systems. 51:1111-1122
Nonlinear guidance laws that consider impact time constraints are proposed. Two-dimensional and three-dimensional impact time control guidance laws are derived using Lyapunov stability theory. Under the consideration of the nonlinear kinematics, it i