|Units or mass||3U|
|Organisation||Astronautic Technology (M) Sdn. Bhd.|
Demonstrate various attitude control algorithms.
To develop Satellite Attitude Control Systems Algorithms: Adaptive Fuzzy Logic Controller and Adaptive Parametric Black Box. Space Experimental Attitude Determination Sensors and solar Panel Sun Sensor (SEADS & SPSS). Pyramid sun sensor, magnometer, and solar panel sensory system to detect and compute body rate and attitude of Satellite. Wireless Sensor Network Payload for InnoSAT Satellite. To develop a Wireless Sensor Network that is operated from a remote location whose data is accessed via InnoSAT and transferred to the main station. Spaceborne Global Positioning System (GPS) Receiver for Autonomous Precise Timing, Positioning, and Navigation. To develop a satellite navigation and positioning system based on GPS.