Closed-loop atmospheric ascent guidance based on finite element method

Author:

Lu Baogang,Cui Naigang,Fu Yu,Shan Wenzhao,Chang Xiaohua

Publisher

Emerald

Reference8 articles.

1. Finite element solution of optimal control problems with state-control inequality constraints

2. Finite Element and Runge-Kutta Methods for Boundary-Value and Optimal Control Problems

3. Chen, G. , Fu, Y. and Guo, J.F. (2011), “Survey of aircraft trajectory optimization methods”, Flight Dynamics , Vol. 29 No. 4, pp. 1-5.

4. Hanson, J.M. , Shrader, M.W. and Cruzen, C.A. (1995), “Ascent guidance comparisons”, Journal of the Astronautical Sciences , Vol. 43 No. 3, pp. 307-326.

5. Weak Hamiltonian finite element method for optimal control problems

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