Hi,
Just first part is needed.
Ok, you would have to complete it using Theory of plane stress elasticity in cartesian co-ordinate systems rather than using finite element analysis, and provide all workings (handwritten would be fine).
MATLAB ASSIGNMENTS COMPLETED
NAVIGATION ASSIGNMENTS
1. 3D Great Circle path generation from one location on Earth to another.
SPACE FLIGHT MECHANICS ASSIGNMENTS
1. Computation of Right ascension and declination angle of Sun for an entire year
2. Transfer orbit generation of a satellite from Low earth orbit to Geostationary orbit
3. Determination of Ground based antenna angles for tracking any satellite
4. Determination of Antenna azimuth and elevation gimbal rates required to track any satellite
5. Orbit determination of Satellite in 3D ECI frame.
$25 USD за 3 дні(-в)
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