Examples on Unit 1 for Practice
Link for quiz4 AIDC WEEK 2 OL 4 pls copy link and paste in browser https://forms.gle/tkFixsqv9KoaV7mp6
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Satellite Orbital Mechanics
Satellite Orbital Mechanics Quiz Q.1) Orbit has eccentricity of 0.15 and semi major axis of 9000 km. Determine Periodic time and Apogee height. Q.2) For a satellite perigee & apogee height is 300 km and 42000 km respectively. Find velocities at apogee & perigee by assuming earth radius 6378 km. Q.3) Sum & difference of apogee and perigee distances are 50000 km & 30000 km for a certain elliptical satellite orbit. Determine eccentricity. Q.4) If apogee height and perigee height is of 39342 km & 613 km. Determine semi major axis & eccentricity. (Src : Satellite Comm. – R P khan) Link To Submit Answers Orbital Mechanics Answer Submission
Link for quiz 3 AIDC WEEK 1 OL 3 pls copy link and paste in browser https://forms.gle/nAcmYdp255vh2H2B7
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