AE40005: Space Dynamics

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AE40005
Course name Space Dynamics
Offered by Aerospace Engineering
Credits 3
L-T-P 3-0-0
Previous Year Grade Distribution
1
3
3
8
8
4
1
EX A B C D P F
Semester Autumn


Syllabus[edit | edit source]

Syllabus mentioned in ERP[edit | edit source]

Prerequisites: AE21003 3 - 0 - 0: 3 Credits N-body problem, ideal two-body equation of motion, Orbit established from initial conditions, Orbital elements, determination of orbits from position and velocity vectors, and from two and three-position vectors, effect of small impulses on orbital elements, Ballistic missile trajectories and performance low acceleration orbit transfers; Equations of motion of a rigid rocket, powered flight trajectory, trajectory optimization, multi-staging and optimization of number of stages. Disturbing forces and control forces, motion of spinning and fin-stabilized rockets, general theory of orbital perturbation and orbit decay, error analysis, Altitude dynamics, Restricted 3-body problem, stability of liberation points, Lunar transfer of orbits, Interplanetary flight.


Concepts taught in class[edit | edit source]

Student Opinion[edit | edit source]

How to Crack the Paper[edit | edit source]

Classroom resources[edit | edit source]

Additional Resources[edit | edit source]


Time Table[edit | edit source]

Day 8:00-8:55 am 9:00-9:55 am 10:00-10:55 am 11:00-11:55 am 12:00-12:55 pm 2:00-2:55 pm 3:00-3:55 pm 4:00-4:55 pm 5:00-5:55 pm
Monday 2nd Year Class Room 2nd Year Class Room
Tuesday 2nd Year Class Room
Wednesday
Thursday
Friday