Author:
Zhang Q.Z.,Wang Z.B.,Tao F.,Sarker Bhaba R.
Funder
National Science and Technology Support Program of China
Subject
Applied Mathematics,Modelling and Simulation
Reference65 articles.
1. Terminal guidance for impact attitude angle constrained flight trajectories;Kim;IEEE Trans. Aerosp. Electron. Syst.,1973
2. Impact angle control for planar engagements;Song;IEEE Trans. Aerosp. Electron. Syst.,1999
3. C.K. Ryoo, H. Cho, M.J. Tahk, Closed-form solutions of optimal guidance with terminal impact angle constraint, in: Proceedings of the IEEE Conference on Control Applications, 2003, pp. 504–509.
4. Y. Lee, C.K. Ryoo, E. Kim, Optimal guidance with constraints on impact angle and terminal acceleration, in: AIAA Guidance, Navigation, and Control Conference, Austin, TX, Aug. 2003.
5. Optimal guidance laws with terminal impact angle constraint;Ryoo;AIAA J. Guidance Control Dyn.,2005
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