This project was successfully completed by okeysir229 for $66 USD in 3 days.

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$30 - $80 USD
Completed In
3 days
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Project Description

The initial condition can be an input for feeding the orbital slot of the Geo
stationary satellite, calculate the azimuth and elevation (satellite look angles) point the
antenna to it. introduce roll pitch and yaw to it. this can be as a continuous sine wave of max
for roll and pitch varying from +- 20 deg period of 5 to 10 sec and yaw +- 10 deg period of 5
sec. then we show that the antenna is pointing making a zig zag pattern etc. then we introduce
the corrections and we should get a steady line from the antenna to the satellite with minor
variations on account of lag / noise etc.

Base SIMULINK cose is done see the attchmnet some extra code addition to attached code is required to create required results

AS per Project_description+%281%[url removed, login to view] SIMULINK code [url removed, login to view] is done , now as per above input condition outputs need to be generated, suitable stabilization code may be added as required

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