飛行控制

Flight Control

飛行控制組的主要任務是要建立衛星姿軌控制與飛行軟體軟、硬體相關次系統與關鍵元件的自主研發能量，以支援下一代遙測衛星與微衛星計畫，並主導或支援福衛二號與三號的姿軌控制備援方案、運轉維護與後續計畫。飛行控制組的工作主軸分為「衛星計畫」、「內部研發」與「對外服務」，此三項工作分頭並進，依序進行。今（2009）年度飛行控制組的主要研發成果包括：（一）與STK介面結合，3D呈現的姿軌控制動態模擬平台、（二）飛行軟體功能驗證平台、等次系統驗證平台開發、（三）『太空級衛星導航接收機』、『抗輻射光纖光源與陀螺儀研發』等關鍵元件研製以及磁矩校準方法的發明專利等。 The core technologies of the Flight Control(FC) division are sub-system software and hardware associated withAttitude and Orbital Control System(AOCS), and Flight Software. The primary mission of FCis to establish independentresearch capabilities in key components and sub-systems and thus support the development of next generationremote-sensing satellites and micro-satellites. Additionally, FC supports and maintains the existing FORMOSAT-2and -3 satellites, their AOCS backup plans and follow-on programs. The daily operations of FC involve performingprogramming, research, and service activities in parallel with satellite programs having the highest priority in mind.The main research accomplishments during 2009 involved three areas: development platforms, key components, andpatents. With regard to development platforms, accomplishments included a 3D AOCS Dynamic Simulator linked toSTK, and a Flight Software Functional Validation Bench(FVB) . Regarding key components, achievements includeddemonstrating performance in Space-Borne GNSS Receiver and Radiation Hardened Fiber Light Source and OpticalGyros. Regarding patent applications, an invention patent entitled Residual Magnetic Dipole Compensation under thePresence of Induced Magnetism was awarded by the Intellectual Property Office of Taiwan. For detailed description ofthe above accomplishments of FC, refer to the Special Topics, and Patents sections of this annual report.