Research Project
Grant-in-Aid for Young Scientists (B)
Using a recently developed technique based on Hamilton-Jacobi theory, we develop a method to approximate the solution of the Hamilton-Jacobi equation which can solve nonlinear trajectory optimization of spacecraft. The proposed method is based on the successive approximation and Galerkin spectral method with Chebyshev polynomials. This approach is expected to derive the analytical solution of the optimal control problem in the large domain.
All 2010 2009
All Journal Article (8 results) (of which Peer Reviewed: 8 results) Presentation (18 results)
Aerospace Technology Japan Vol.8, No.ists27
Pages: 9-13
Advances in the Astronautical Sciences Vol.136
Pages: 587-603
AIAA Journal of Guidance, Control, and Dynamics Vol.33 No.3
Pages: 1000-1008
Advances in the Astronautical Sciences
Volume: 136 Pages: 587-603
Transactions of the Japan Society for Aero nautical and Space Sciences, Aerospace Technology Japan
Volume: 8
130000675480
AIAA Journal of Guidance, Control, and Dynamics 33
Advances in the Astronautical Sciences Vol.134
Pages: 245-260
120007044555
Advances in the Astronautical Sciences 134