InnoSAT Satellite

Name InnoSAT
Spacecraft type CubeSat
Units or mass 3U
Status cancelled
Organisation ATSB (Astronautic Technology Sdn Bhd)
Institution Company
Entity Commercial
Headquarters Malaysia
Partners Universiti Sains Malaysia (USM), Universiti Teknologi Malaysia (UTM) and Universiti Malaysia Perlis (UniMAP).

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.

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Last modified: 2024-05-29

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Created by Erik Kulu


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