摘要
针对在轨航天器主动防护的问题,文章综合考虑了未来航天器规避原则和规避过程中可能出现的因素,提出了在轨航天器轨道规避体系的构造思路。根据规避对象为空间碎片和航天器时的情况,建立了相应的规避基础框架;并利用事例对其中一个基础框架进行了分析和验证。分析结果表明,在轨航天器规避框架的研究对于降低航天器潜在威胁、增强航天器在轨运行安全具有积极的作用。
Aim. To our knowledge, Ref. 5 authored by K. R. Keagan is the only paper in the open literature dealing with many aspects of the topic mentioned in the title. Starting from Ref. 5, our exploration goes further. Table 1 in subsection 1.2 of the full paper presents as usual the three stageε of OSCAF design but Lheir contents include the resuits of our exploration. Fig. 1 in subsection 2.1 presents the block diagram of OSCAF design for spacecraft versus debris and Fig. 2 also in subsection 2.1 presents that for spacecraft versus spacecraft. Section 3 presents an example concerning spacecraft versus spacecraft. Table 2 in section 3 gives the information about the conditions under which two spacecraft collide. Possessing such information can ensure the avoidance of the collision of two spacecraft.
出处
《西北工业大学学报》
EI
CAS
CSCD
北大核心
2010年第1期13-17,共5页
Journal of Northwestern Polytechnical University
关键词
轨道规避框架
规避体系
规避机动
主动防护
在轨安全
spacecraft, orbital collision, collision avoidance, on-orbit spacecraft collision avoidance framework (OSCAF)