卫星多机构一体式高效展开试验方法
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国防基础科研项目(JCKY2020203B039)


Satellite Multi-mechanism Integrated and Efficient Deployment Test Method
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    摘要:

    为减少卫星姿态转换和试验状态反复建立,提高卫星空间机构展开测试效率,提出一种卫星多机构一体式高效展开试验方法。采用星载式重力卸载新模式、多机构一体式展开方法,开展卫星-装置一体化展开试验设计、多机构空间力学耦合分析、运动学及动力学分析、展开锁定冲击影响以及展开型面精度分析等,完成多机构一体式地面展开试验验证。结果表明:相比传统试验方法,该方法能更真实地模拟卫星在轨展开时序和展开状态;机构重复展开测试数据一致性较好,展开试验效率更高;可广泛应用于批产卫星的高效、高质量研制。

    Abstract:

    In order to reduce satellite attitude conversion and repeated establishment of test state, and improve the efficiency of satellite space mechanism deployment test, an efficient deployment test method of satellite multi-mechanism integration was proposed. By adopting the new mode of satellite-borne gravity unloading and the multi-mechanism integrated deployment method, the satellite-device integrated deployment test design, multi-mechanism space mechanics coupling analysis, kinematics and dynamics analysis, the impact of deployment locking and the accuracy analysis of deployment profile are carried out, and the multi-mechanism integrated ground deployment test verification is completed. The results show that, compared with the traditional test method, this method can simulate the deployment sequence and deployment state of the satellite in orbit more realistically; the consistency of the repeated deployment test data of the mechanism is better, and the deployment test efficiency is higher; it can be widely applied to the efficient and high-quality development of the batch production satellite.

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刘晓飞.卫星多机构一体式高效展开试验方法[J].,2026,45(02).

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  • 收稿日期:2024-11-07
  • 最后修改日期:2024-12-09
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  • 在线发布日期: 2026-03-13
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