本論文為探討 珍珠號（ Propagation Experiment Using Kurz-Above-Band Radio in Low Earth Orbit,PEARL立方衛星的結構設計與模擬。 PEARL-1C立方衛星計畫為國立中央大學太空酬載實驗室所主導的 低軌寬頻 通訊 實驗 採用 保加利亞 EnduroSat的衛星本體 。 各酬載與次系統 按照EnduroSat的固裝 方式，由中大自行 整合與組裝。 藉由模擬 分析 ，按照發射服務公司提供的環境測試規格，確認該本體能符合環境測試規範。 本文所使用的模擬軟體為 SolidWorks內建的SolidWorks Simulation功能，模 擬項目有自然頻率測試、加速度測試、隨機振動測試、外力 負載 測試 、 正弦振動測試 、 衝擊測試 。;The main purpose of this thesis is to verify the design of Propagation Experiment Using Kurz-Above-Band Radio in Low Earth Orbit (PEARL) CubeSat structural. The PEARL-1C CubeSats are a communication satellite experiment led by Space Payload Laboratory, National Central University The PEARL bus structure is designed and manufactured by a Bulgarian company, EnduroSat. The Space Payload Laboratory is self-produced and will simulate and study the satellite structure of EnduroSat and apply it to the PEARL-1H satellite structure. The simulation software used in this article is the built-in SolidWorks Simulation function of SolidWorks. The simulation items include: natural frequency test, acceleration test, random vibration test, external force attached test, Sine Vibration, shock. In terms of installation, each payload and sub-system must meet the fixed method of EnduroSat satellite design, and can be assembled according to a certain installation sequence.
