AEE462 Lecture 8, Part A - Delta V and Transfer Orbits
AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit
AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem
AEE462 Lecture15a - Introduction to Spacecraft Design
AEE462 Lecture 10, Part C - A Bisection Algorithm for the Solution of Lambert's Equation
AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers
AEE462 Lecture 7, Part A - A Summary of the Method for Orbit Propagation
AEE462 Lecture 9, Part A - The Oberth Effect
Lecture 8 Central Force Motion and Space Mechanics
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 9, Part B - Bi-Elliptic Transfers
AEE462 Lecture 9, Part C - Orbital Plane and Launch Geometry: Azimuth, Inclination, and Lattitude
AEE462 Lecture 3, Part C - Proving Kepler's 2nd and 3rd Law and Turning Angle for Hyperbolic Orbits
AEE462 Lecture 3, Part A - The Eccentricity Vector and the Polar Equation
AEE462 Lecture 1, Part D - Kepler's 3 Laws of Planetary motion and Newton's Universal Gravitation
RxV to COEs: The How-To Guide
AEE462 Lecture 1, Part C - Orbits and the Scientific Revolution
Phase Angle for circular orbits with Hohmann transfer
InSPIRESS Physics Calculations: De-Orbit
