论文信息 - Indirect Spacecraft Trajectory Optimization Using Modified Equinoctial Elements - 字舞流文

Indirect Spacecraft Trajectory Optimization Using Modified Equinoctial Elements

Benson H. Tongue | Hongzhao Liu

[1] Jean Albert Kechichian. Minimum-Time Constant Acceleration Orbit Transfer with First-Order Oblateness Effect , 2000 .

[2] Anil V. Rao,et al. Practical Methods for Optimal Control Using Nonlinear Programming , 1987 .

[3] D. D. Mueller,et al. Fundamentals of Astrodynamics , 1971 .

[4] M. J. Walker. A set of modified equinoctial orbit elements , 1985 .

[5] Gerald R. Hintz,et al. Survey of Orbit Element Sets , 2008 .