{'fraction_non_alphanumeric': 0.02120141342756184, 'fraction_numerical': 0.0, 'mean_word_length': 5.670588235294118, 'pattern_counts': {'":': 0, '<': 0, '<?xml version=': 0, '>': 0, 'https://': 0, 'lorem ipsum': 0, 'www.': 0, 'xml': 0}, 'pii_count': 0, 'substrings_counts': 0, 'word_list_counts': {'cursed_substrings.json': 0, 'profanity_word_list.json': 0, 'sexual_word_list.json': 0, 'zh_pornsignals.json': 0}}
Optimal Control of Fully-Actuated Systems for Spacecraft Rendezvous

In this paper, the rigid spacecraft rendezvous problem is studied in the sense of fully-actuated system. According to the attitude and orbit dynamics, the fully-actuated system model is established. And the linear quadratic optimal controller of the fully-actuated system is designed for spacecraft rendezvous task. Finally, numerical simulation and physical experiment are considered. Both simulation and experiment results indicate the effectiveness and practicability of the optimal controller.