Lambert's problem for exponential sinusoids

D Izzo - Journal of guidance, control, and dynamics, 2006 - arc.aiaa.org
LOW-THRUST trajectories are becoming increasingly impor-tant in the design of space
missions. The technological developments that allowed ion propulsion to become a …

A framework of gravity field online modeling and trajectory optimization in asteroid soft-landing mission scenarios

W Feng, M Huo, Y Xu, L Mo, W Ke, Y Ma, H Su… - Aerospace Science and …, 2023 - Elsevier
Focused on asteroid soft-landing mission scenario, this paper investigates the methods of
online gravity field modeling and trajectory optimization. Since the gravity field near …

New look to the constant radial acceleration problem

AA Quarta, G Mengali - Journal of guidance, control, and dynamics, 2012 - arc.aiaa.org
IN RECENT years, considerable attention has been devoted to the problem offinding
innovative trajectories for spacecraft subjected to a low-thrust propulsion system. The focus …

[PDF][PDF] Spiral trajectories in global optimisation of interplanetary and orbital transfers

M Vasile, O Schütze, O Junge, G Radice… - Ariadna study report …, 2006 - researchgate.net
NASA's Deep Space 1 and recently ESA's SMART-1 have shown the effectiveness of
lowthrust systems as primary propulsion devices. This opens the door to new kinds of …

Initial three-dimensional trajectory design for solar sails using Bezier shaping approach

M Huo, Z Yu, H Liu, C Zhao, T Lin, Z Song, N Qi - IEEE Access, 2019 - ieeexplore.ieee.org
An approach for the fast generation of a minimum-time, three-dimensional trajectory for a
spacecraft propelled by a solar sail with reflection control devices (RCDs) is presented using …

A hybrid genetic algorithm approach to global low-thrust trajectory optimization

MA Vavrina - 2008 - search.proquest.com
To expand mission capabilities that are required for exploration of the solar system,
methodologies to design optimal low-thrust trajectories must be developed. However, low …

Rapid Trajectory Optimization of Continuous-Low-Thrust Spacecraft Based on Bezier Shape Function and Inverse Dynamics

T Wang, X Shang, J Wang, M Huo, N Qi - International Conference on …, 2023 - Springer
Deep space exploration missions are a great fit for continuous-thrust spacecraft because of
their benefits of high specific impulse and extended operating period. However, when it …

Subspace optimal control and motion camouflage

Y Xu - AIAA Guidance, Navigation and Control Conference …, 2008 - arc.aiaa.org
Some insects can move towards female ones or their preys while minimizing the chance of
being aware from their natural background using a technique called motion camouflage. In …

[引用][C] 基于轨迹成型法星际小推力转移轨道快速设计

叶立军, 孟占峰, 韩潮 - 航天控制, 2009