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NORTH AND SOUTH ORBIT CONTROLLING METHOD USING LOW THRUST THRUSTER

机译:低推力推力的南北轨道控制方法

摘要

PURPOSE: To minimize the reduction of control efficiency when there is a forbidden band by providing an orbital inclination angle for a node to keep it constant in an inertial space, and executing injections at the location nearest to the node outside the forbidden band, or providing an orbital inclination angle of 0 degree, and executing injections at the location which is expected to provide the best efficiency regardless of the node. ;CONSTITUTION: A node 11 is provided with a certain orbital inclination angle and is kept almost constant in an inertial space. Based on the positional relationship between a forbidden band 12 and the node 11, a thruster executes injections 10 on the node 11 when the forbidden band 12 is out of the node 11, while it executes injections 10 at the position nearest to the node 11 outside the forbidden band 12 when the band 12 is on the node 11. With the rotation of the node 11 caused by the injections taken into consideration, injections 10 start at one position outside the forbidden band and end at a proper position and then are executed at both front and rear of the band 12. In addition, an orbital inclination angle of 0 degree is provided and injections 10 are executed at the position which is expected to provide the best efficiency regardless of the node 11.;COPYRIGHT: (C)1993,JPO&Japio
机译:目的:通过为节点提供轨道倾斜角以使其在惯性空间中保持恒定,并在禁带外最靠近该节点的位置执行注入,或轨道倾角为0度,并在与节点无关的预期位置提供最佳喷射。组成:节点11具有一定的轨道倾角,并且在惯性空间中几乎保持恒定。基于禁带12与节点11之间的位置关系,推力器在禁带12离开节点11之外时在节点11上执行注入10,而在外部最靠近节点11的位置处执行注入10。当禁带12位于节点11上时,禁带12处于禁区12。考虑到由注入引起的节点11的旋转,注入10在禁带之外的一个位置开始并在适当的位置结束,然后在频带12的前后。此外,提供了0度的轨道倾角,并且在与节点11无关的预期提供最佳效率的位置处执行注入10; COPYRIGHT:(C)1993 ,JPO&Japio

著录项

  • 公开/公告号JPH05155398A

    专利类型

  • 公开/公告日1993-06-22

    原文格式PDF

  • 申请/专利权人 MITSUBISHI ELECTRIC CORP;

    申请/专利号JP19910322938

  • 发明设计人 YUZAWA MARI;

    申请日1991-12-06

  • 分类号B64G1/26;

  • 国家 JP

  • 入库时间 2022-08-22 05:16:42

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