In Progress

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

Skills: Algorithm, Electrical Engineering, Engineering, Mathematics, Matlab and Mathematica

See more: orbital engineering, elevation engineering, mathematica show, zig, simulink matlab, mdl, matlab/simulink, matlab simulink, MATLAB and SIMULINK, matlab + it, bchandra1955, azimuth, minor corrections, matlab support, support matlab, antenna simulink, pitch period matlab, support line, simulink antenna, antenna pattern, matlab antenna simulink, pattern matlab, stabilization, elevation max, max elevation

Project ID: #4479996

Awarded to:


I have a lot of experiences at matlab, and verry good at math. You can see in my profile. Just hire me to do it for you.

$66 USD in 3 days
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