AEE462 Lecture 7, Part A - A Summary of the Method for Orbit Propagation
AEE462 Lecture 7, Part C - Using Orbital Elements to Find Position and Velocity Vectors
AEE462 Lecture 8, Part A - Delta V and Transfer Orbits
AEE462 Lecture 7, Part B - A Review of Rotation Matrices and Conversion between Coordinate Systems
LSN 7 - Classical Orbital Elements (COE) Definitions
ASEN 5148 Spacecraft Design - Sample Lecture
AEE462 Lecture 6, Part A - Coordinate Systems in Space
AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem
AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time
RxV to COEs: The How-To Guide
LSN 9 - Transforming a Position Vector and a Velocity Vector into the 6 Classical Orbital Elements
AEE462 Lecture 10, Part B - Lambert's Equation and the Solution to Lambert's Problem
AEE462 Lecture 1, Part A/B - Orbits and the Greeks
AEE462 Lecture 7, Part D - Right Ascension, Declination, and Local Sidereal Time
AEE462 Lecture 6, Part B (rev 1) - 3D Orbital Elements: Inclination, RAAN, and Argument of Periapse
AEE462 Lecture 9, Part C - Orbital Plane and Launch Geometry: Azimuth, Inclination, and Lattitude
AEE462 Lecture 1, Part D - Kepler's 3 Laws of Planetary motion and Newton's Universal Gravitation
AEE462 Lecture 9, Part A - The Oberth Effect
LSN 21 - Launch Windows
AEE 462 Lecture 12 - Orbital Perturbations and Atmospheric Drag
