Tangent-impulse transfer from elliptic orbit to an excess velocity vector

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• 作者：Gang Zhang^a ; ^b ; ^{zhanggang@hit.edu.cn" class="auth_mail}Author Vitae ; Xiangyu Zhang^a ; ^{zxyuhit@gmail.com" class="auth_mail}Author Vitae ; Xibin Cao^a ; ^b ; ^{xbcao@hit.edu.cn" class="auth_mail}Author Vitae
• 关键词：Elliptic orbit ; Escape trajectory ; Excess velocity vector ; Orbital transfer ; Tangent impulse
• 刊名：Chinese Journal of Aeronautics
• 出版年：June 2014
• 年：2014
• 卷：27
• 期：3
• 页码：577-583
• 全文大小：863 K

文摘

The two-body orbital transfer problem from an elliptic parking orbit to an excess velocity vector with the tangent impulse is studied. The direction of the impulse is constrained to be aligned with the velocity vector, then speed changes are enough to nullify the relative velocity. First, if one tangent impulse is used, the transfer orbit is obtained by solving a single-variable function about the true anomaly of the initial orbit. For the initial circular orbit, the closed-form solution is derived. For the initial elliptic orbit, the discontinuous point is solved, then the initial true anomaly is obtained by a numerical iterative approach; moreover, an alternative method is proposed to avoid the singularity. There is only one solution for one-tangent-impulse escape trajectory. Then, based on the one-tangent-impulse solution, the minimum-energy multi-tangent-impulse escape trajectory is obtained by a numerical optimization algorithm, e.g., the genetic method. Finally, several examples are provided to validate the proposed method. The numerical results show that the minimum-energy multi-tangent-impulse escape trajectory is the same as the one-tangent-impulse trajectory.