AEE462 Lecture 4, Part B - Newton-Raphson Iteration and Kepler's Equation
AEE462 Lecture 6, Part B (rev 1) - 3D Orbital Elements: Inclination, RAAN, and Argument of Periapse
AEE462 Lecture 4, Part A - Moving Elliptic Orbits in Time
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 3, Part C - Proving Kepler's 2nd and 3rd Law and Turning Angle for Hyperbolic Orbits
AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time
AEE462 Lecture 3, Part B - Parameters of Elliptic and Hyperbolic Motion
AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers
AEE462 Lecture 9, Part B - Bi-Elliptic Transfers
AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit
AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem
AEE462 Lecture 9, Part C - Orbital Plane and Launch Geometry: Azimuth, Inclination, and Lattitude
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 A - A Summary of the Method for Orbit Propagation
4 - 4 - Lambert's Time of Flight Theorem
5 - 4 - Impulsive Maneuvers and Co-Planar Orbital Transfers
AEE462 Lecture 6, Part A - Coordinate Systems in Space
AEE462 Lecture 3, Part A - The Eccentricity Vector and the Polar Equation
