摘要
结合干涉成像原理与空间探测中的编队飞行技术,提出一种空间干涉测量成像的方案。首先,建立了基于编队干涉技术的测量成像系统结构,利用ASPRO软件,通过建模和仿真分析了主要系统参数对UV覆盖性能的影响;然后,基于编队干涉系统,针对月球探测任务设计了一种低能耗、高灵活性的干涉成像方案;最后,利用所提方案对目标天体的测量成像进行了模拟重构和仿真分析。所提方案为下一步空间干涉测量任务的设计提供了一定参考。
A novel idea of blending celestial imaging concept is proposed with the interferometry principle and the formation flying technology for image reconstruction.The formation flying based on interferometry imaging structure is described in details.The effects of the main system parameters on the UV coverage are analyzed and simulated by virtue of the ASPRO software.A low fuel-cost and highly flexible interferometry scheme is proposed for the moon exploration task related to object image reconstruction,with simulations and analysis.The proposed scheme is of value for future space exploration.
出处
《控制工程》
CSCD
北大核心
2010年第S1期104-106,共3页
Control Engineering of China
关键词
编队干涉
空间探测
测量成像
控制方案
模拟重构
formation interferometry
space exploration
measurement imaging
control scheme
reconstruction and simulation
