中文摘要 |
飛行控制組的任務包含建立衛星姿態控制與飛行軟體兩個次系統的完整能量、主導關鍵導航與控制元件的研製及建立航太製作工藝與測試能量,以支援本中心與國內的衛星計畫發展,並支援福衛二號與福衛三號的運轉維護與問題排除。2011年飛行控制組完成或精進的主要研發成果計有,完成福衛五號姿控測試器驗證與初步姿控閉迴路測試、完成福衛五號飛行軟體重大改版並完成此版飛行軟體的姿控功能驗證、完成數項太空級導航接收機關鍵技術驗證、更新「電磁相容與天線測試實驗室」設備並取得全國實驗室認證基金會的認證、與取得美國太空總署「衛星電子組件聚合物運用」之工藝技術能量。
To support the NSPO and domestic satellite projects, including operation and emergency response for existingFORMOSAT-2 and 3, the Flight Control Division(FCD) needs to establish necessary capability for satelliteattitude control and flight software subsystems, develop key navigation and control components, upgrademanufacturing workmanship to aerospace-grade and acquire necessary testing facility for validation. In 2011, those credible accomplishments or advancement that FCD deliver includes the validation of FORMOSAT-5Attitude and Orbit Control Subsystem(AOCS) test bed, preliminary AOCS loop closure test, major revision forFORMOSAT-5 Flight Software(FSW) and associated AOCS functional test, validation of several key technologiesfor space-grade GPSR, refurbishment of EMC(Electromagnetic Compatibility) and Antenna Test Lab instrumentsand its accreditation from Taiwan Accreditation Foundation(TAF), Technology transfer of Polymeric Applicationon Electronic Assemblies from NASA. |