AEE462 Lecture 10, Part B - Lambert's Equation and the Solution to Lambert's Problem
AEE462 Lecture 10, Part C - A Bisection Algorithm for the Solution of Lambert's Equation
AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem
AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit
Calculate Transit Time to Change Orbit in a Hohmann Transfer
AEE462 Lecture 9, Part B - Bi-Elliptic Transfers
Orbital Mechanics - Preliminary Orbit Determination and Lambert's Problem
AEE462 Lecture 4, Part B - Newton-Raphson Iteration and Kepler's Equation
Phase Angle for circular orbits with Hohmann transfer
AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers
Learn about Elliptic Orbit (energy, geometry, orbit velocity, eccentricity, semilatus rectum)
Multibody Dynamics B, ME41055, Lecture 10, part 1, Thu 23 May 2019
AEE462 Lecture 8, Part A - Delta V and Transfer Orbits
AEE462 Lecture 9, Part C - Orbital Plane and Launch Geometry: Azimuth, Inclination, and Lattitude
4 - 4 - Lambert's Time of Flight Theorem
AEE462 Lecture 6, Part B (rev 1) - 3D Orbital Elements: Inclination, RAAN, and Argument of Periapse
AERO4540 - Spacecraft Attitude Dynamics and Control - Lecture 10
AEE462 Lecture 3, Part C - Proving Kepler's 2nd and 3rd Law and Turning Angle for Hyperbolic Orbits
MAE509 (LMIs in Control): Lecture 3 - Convex Cones, Duality, LMIs
AEE 462 Lecture 12 - Orbital Perturbations and Atmospheric Drag
