Overview - Space Flight mechanics
Two body problem - Equation of relative motion
Conservation of angular momentum and Kepler's second law
Orbit equation
Parameters of Orbit equation and The Energy law
Circular orbits
Elliptical orbits
Problems on Elliptical orbits
Parabolic trajectories
Hyperbolic trajectories
Problems on hyperbolic orbits
Introduction to orbital maneuvers
Hohmann Transfer
Problems on Hohmann transfer
Bi-elliptic Hohmann transfer
Lambert problem - Satellite tracking
Eccentric anomaly (Satellite tracking)
Phasing maneuver
Inclination change maneuver
Combined maneuver & Launch azimuth
Problems on combined maneuver
Introduction to Lunar/Interplanetary trajectory design
Rendezvous opportunities (Synodic period)
Round-trip mission (Wait time)
Sphere of Influence
Method of trajectory design (Departure phase)
Method of trajectory design (Arrival phase)
Problems (Part 1)
Problems (Part 2)
Problems (Part 3)
Restricted three body problem
Lagrangian points
Non-Keplerian motion
Atmospheric drag
Orbital lifetime of a spacecraft - Examples
Earth aspherical potential
Radiation pressure & Third body effects
Application of orbital perturbations - Sun synchronous orbits
Application of orbital perturbations - Molniya orbits
Rigid body dynamics - Attitude control
