InnoSAT

ATS-10 Satellite Bus Systems Developed by ATSB^® and experimental payloads developed by 4 local universities:

UNIMAP (Universiti Malaysia Perlis)

Attitude Control System (ACS)
To develop Satellite Attitude Conteol Systems Algorithms: Adaptive Fuzzy Logic Controller  and Adaptive Parametric Black Box.

USM (Universiti Sains Malaysia)

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.

UTM (Universiti Teknologi Malaysia)

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