InnoSAT

InnoSAT
Name InnoSAT
Type CubeSat
Units or mass 3U
Status cancelled
Organisation Astronautic Technology (M) Sdn. Bhd.
Institution Company
Entity Commercial
Nation Malaysia
Oneliner

Demonstrate various attitude control algorithms.

Description

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.

Sources [1] [2]
Photo Sources [1]

Last modified: 2022-12-29
Detailed InnoSAT entry in the Database
Full Nanosats Database (much more data)

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Created by Erik Kulu

Email: erik.kulu@nanosats.eu
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