AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time
5 - 4 - Impulsive Maneuvers and Co-Planar Orbital Transfers
AEE462 Lecture15a - Introduction to Spacecraft Design
AEE462 Lecture 10, Part C - A Bisection Algorithm for the Solution of Lambert's Equation
AEE462 Lecture 6, Part B (rev 1) - 3D Orbital Elements: Inclination, RAAN, and Argument of Periapse
MAE509 (LMIs in Control): Lecture 5, part A - Controllability and the Grammian
AEE462 Lecture 6, Part A - Coordinate Systems in Space
Space Mechanics | Orbital Maneuver | Plane Change Maneuver
AEE462 Lecture 7, Part A - A Summary of the Method for Orbit Propagation
AEE462 Lecture 1, Part A/B - Orbits and the Greeks
AEE462 Lecture 4, Part B - Newton-Raphson Iteration and Kepler's Equation
AEE462 Lecture 10, Part B - Lambert's Equation and the Solution to Lambert's Problem
AEE462 lecture 14c - Gravitational Assist Maneuvers
AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers
GCSVS Module 3 - Orbital transfer - Part 2 - Combined Plane Change Example
LSN 9 - Transforming a Position Vector and a Velocity Vector into the 6 Classical Orbital Elements
AEE462 Lecture 4, Part A - Moving Elliptic Orbits in Time
ASEN 5148 Spacecraft Design - Sample Lecture
AEE462 Lecture 1, Part D - Kepler's 3 Laws of Planetary motion and Newton's Universal Gravitation
Orbital Motion in Cislunar Space
