AEE462 Lecture 2, Part B - The 2 body problem, gravitational constants and Energy Cons. Examples
AEE462 Lecture 3, Part B - Parameters of Elliptic and Hyperbolic Motion
AEE462 Lecture 10, Part B - Lambert's Equation and the Solution to Lambert's Problem
AEE462 Lecture 6, Part B (rev 1) - 3D Orbital Elements: Inclination, RAAN, and Argument of Periapse
AEE462 Lecture 9, Part B - Bi-Elliptic Transfers
AEE462 Lecture 1, Part A/B - Orbits and the Greeks
AEE462 Lecture 2, Part A - The N-body Problem and Physical Invariants
AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time
AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit
Space Mechanics | Orbital Maneuver | Bi-elliptic Transfer
AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem
AEE462 Lecture 10, Part C - A Bisection Algorithm for the Solution of Lambert's Equation
AEE462 Lecture15a - Introduction to Spacecraft Design
Astrodynamics UF lecture2
AEE462 Lecture 4, Part B - Newton-Raphson Iteration and Kepler's Equation
AEE462 Lecture 1, Part C - Orbits and the Scientific Revolution
AEE462 Lecture 3, Part C - Proving Kepler's 2nd and 3rd Law and Turning Angle for Hyperbolic Orbits
AEE462 Lecture 9, Part C - Orbital Plane and Launch Geometry: Azimuth, Inclination, and Lattitude
AEE462 Lecture 7, Part A - A Summary of the Method for Orbit Propagation
Mike Gruntman, From Firecrackers to Interstellar Flight. Part 2. Space in 21st Century
