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 Lecture 10, Part B - Lambert's Equation and the Solution to Lambert's Problem
AEE462 Lecture 8, Part A - Delta V and Transfer Orbits
ASEN 5148 Spacecraft Design - Sample Lecture
AEE 462 Lecture 12 - Orbital Perturbations and Atmospheric Drag
Phase Angle for circular orbits with Hohmann transfer
AEE462 Lecture 7, Part A - A Summary of the Method for Orbit Propagation
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
Lecture 10: The DoD and the Space Shuttle (Audio Normalized)
AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers
AERO4540 - Spacecraft Attitude Dynamics and Control - Lecture 10
Impact Of Electrostatic Perturbations On Proximity Operations In High Earth Orbits
AEE462 Lecture 9, Part A - The Oberth Effect
LSN 9 - Transforming a Position Vector and a Velocity Vector into the 6 Classical Orbital Elements
AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit
4 - 4 - Lambert's Time of Flight Theorem
LSN 21 - Launch Windows
Multibody Dynamics B, ME41055, Lecture 10, part 1, Thu 23 May 2019
