When the payload on a spacecraft is installed with the platform, a suitable installation mode should be designed according to the shape of the payload to ensure the reliable connection between the payload and the platform. The payload installed on a spacecraft is elongated. Based on the analysis of the characteristics of this type of payload, this paper designs a installation method between it and the platform, and designs an installation gap adjustment mode. After the installation is completed, the installation can be judged whether the installation is in place by detecting the installation gap between the payload and the platform. The reasonableness and reliability of the designed installation mode are verified by mechanical tests. The test results show that the designed loading installation mode meets the mechanical requirements.
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Wang et al. (2024) studied this question.
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