多功能型混和式火箭是國家太空中心計畫，將安裝中央大學太空酬載實驗室自製任務酬載 - 電離層閃爍儀（Ionosphere Scintillation Package, ISP）， 用來量測臺灣上空電離層E層電漿不規則體結構，以及姿態辨識的比較。其中包括兩台小型電離層探測儀(Compact Ionosphere Probe, CIP)、兩台追星儀(Star Tracker, STR)、及姿態系統（ASM，其中包含兩顆加速計、磁力計、陀螺儀。）為整合上述儀器所蒐集之各個資訊，故採用sbRIO-9607做為控制板，其控制板體積小，擁有多種通訊介面可供使用，並且透過CLIP設定，簡化FPGA的撰寫方式，降低FPGA程式記憶體使用量。用LabVIEW QMH(Queued Message Handler)的架構，讓增加了程式許多的彈性，存取不同的資料更佳的便利，提高程式的易讀性，讓後續維護者容易進行程式的維護，更快達到目的性，來完成任務目標。

The multi-functional hybrid rocket is the National Space Center project, which will install the Ionosphere Scintillation Package (ISP), a self-service mission of the Central University Space Revenue Laboratory, to measure the ionospheric E-layer plasma over Taiwan. Regular body structure, and comparison of pose recognition. These include two Compact Ionosphere Probes (CIPs), two Star Trackers (STRs), and Aspectmeter (ASMs, which include two accelerometers, magnetometers, and gyroscopes). The sbRIO-9607 is used as the control board. The control board is small in size and has a variety of communication interfaces. It can be used to simplify FPGA writing and reduce the amount of FPGA program memory. With LabVIEW QMH (Queued Message Handler) architecture, it adds a lot of flexibility to programs, accesses different data for better convenience, improves program readability, and makes it easier for subsequent maintainers to maintain programs and achieve faster results. To accomplish the mission objectives.

1. Leens, F. (2009). An introduction to I2C and SPI protocols. IEEE Instrumentation & Measurement Magazine, 12(1), 8–13. doi:10.1109/mim.2009.4762946
2. 蔡秉翰，「小型電離層探測儀地面電子測試設備」國立中央大學太空科學研究所，碩士論文，2017
3. 曹智涵，「探空十號火箭的姿態重建與分析」國立中央大學太空科學研究所，碩士論文，2015
4. NI sbRIO-9607 User Manual
5. NI sbRIO-9607/9627 RIO Mezzanine Card Design Guide
6. HMC5883L Datasheet
7. ADXL345 Datasheet
8. L3G4200D Datasheet