阅读说明：本技术 一种充气天线 (Inflatable antenna ) 是由 杜志贵 杨峰 任维佳 向晓霞 于 2019-11-29 设计创作，主要内容包括：本发明涉及一种体积可控的充气天线,至少包括卫星推进器、至少一个获取模块以及至少一个调整模块,第一调整模块被配置为：基于变轨环境监测信息确定第一天线调整控制信息；确定卫星推进器用于执行该特定事件的所需预估消耗量；基于第一天线调整控制信息和预估消耗量确定卫星推进器和充气天线分别对应的变轨需求混合比例系数以及与之对应的第一控制指令和第二控制指令,以使得充气天线的第一调整模块按照对接收第二控制指令的卫星推进器的第二调整模块进行气动力补偿的方式接收第一控制指令,并基于由第二获取模块于第二时刻获取的与该点火变轨位置所涉及区域相关联的第二气动力信息进行至少一次调整修正以执行至少一个相关的特定事件。(The invention relates to a volume-controllable gas-filled antenna comprising at least a satellite thruster, at least one acquisition module and at least one adjustment module, the first adjustment module being configured to: determining first antenna adjustment control information based on the orbital transfer environment monitoring information; determining a desired projected consumption of the satellite propulsor for performing the particular event; and determining a track-transfer demand mixing proportion coefficient corresponding to the satellite thruster and the inflation antenna respectively and a first control instruction and a second control instruction corresponding to the track-transfer demand mixing proportion coefficient based on the first antenna adjustment control information and the estimated consumption, so that a first adjustment module of the inflation antenna receives the first control instruction in a mode of performing aerodynamic compensation on a second adjustment module of the satellite thruster receiving the second control instruction, and performing at least one adjustment correction based on second aerodynamic information, acquired by a second acquisition module at a second moment, associated with an area related to the ignition track-transfer position to execute at least one related specific event.)