AEE462 Lecture 6, Part B (rev 1) - 3D Orbital Elements: Inclination, RAAN, and Argument of Periapse
AEE462 Lecture 10, Part B - Lambert's Equation and the Solution to Lambert's Problem
AEE462 Lecture 7, Part C - Using Orbital Elements to Find Position and Velocity Vectors
AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit
AEE462 Lecture 7, Part A - A Summary of the Method for Orbit Propagation
AEE462 Lecture 4, Part B - Newton-Raphson Iteration and Kepler's Equation
AEE462 Lecture 6, Part A - Coordinate Systems in Space
AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers
AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem
AEE462 Lecture 9, Part B - Bi-Elliptic Transfers
AEE462 lecture 14c - Gravitational Assist Maneuvers
Orbital Motion in Cislunar Space
AEE462 Lecture 7, Part B - A Review of Rotation Matrices and Conversion between Coordinate Systems
AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time
9 - 1 - Central Force Motion in 3D and Delaunay Elements
AEE462 Lecture 4, Part A - Moving Elliptic Orbits in Time
AEE462 Lecture 1, Part D - Kepler's 3 Laws of Planetary motion and Newton's Universal Gravitation
Introduction to Orbital Mechanics Part 1
5 - 4 - Impulsive Maneuvers and Co-Planar Orbital Transfers
LSN 15 - Predicting Orbits
