1 AEE462, Lecture1, Part A - Introduction and Structure of the Course
2 AEE462 Lecture 1, Part B - Orbits and the Greeks
3 AEE462 Lecture 1, Part C - Orbits and the Scientific Revolution
4 AEE462 Lecture 1, Part D - Kepler's 3 Laws of Planetary motion and Newton's Universal Gravitation
5 AEE462 Lecture 2, Part A - The N-body Problem and Physical Invariants
6 AEE462 Lecture 2, Part B - The 2 body problem, gravitational constants and Energy Cons. Examples
7 AEE462 Lecture 3, Part A - The Eccentricity Vector and the Polar Equation
8 AEE462 Lecture 3, Part B - Parameters of Elliptic and Hyperbolic Motion
9 AEE462 Lecture 3, Part C - Proving Kepler's 2nd and 3rd Law and Turning Angle for Hyperbolic Orbits
10 AEE462 Lecture 4, Part A - Moving Elliptic Orbits in Time
11 AEE462 Lecture 4, Part B - Newton-Raphson Iteration and Kepler's Equation
12 AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time
13 AEE462 Lecture 6, Part A - Coordinate Systems in Space
14 AEE462 Lecture 6, Part B (rev 1) - 3D Orbital Elements: Inclination, RAAN, and Argument of Periapse
15 AEE462 Lecture 7, Part A - A Summary of the Method for Orbit Propagation
16 AEE462 Lecture 7, Part B - A Review of Rotation Matrices and Conversion between Coordinate Systems
17 AEE462 Lecture 7, Part C - Using Orbital Elements to Find Position and Velocity Vectors
18 AEE462 Lecture 7, Part D - Right Ascension, Declination, and Local Sidereal Time
19 AEE462 Lecture 8, Part A - Delta V and Transfer Orbits
20 AEE462 Lecture 8, Part B - The Hohmann Transfer Orbit
21 AEE462 Lecture 9, Part A - The Oberth Effect
22 AEE462 Lecture 9, Part B - Bi-Elliptic Transfers
23 AEE462 Lecture 9, Part C - Orbital Plane and Launch Geometry: Azimuth, Inclination, and Lattitude
24 AEE462 Lecture 9, Part D - Orbital Plane-Change Maneuvers
25 AEE462 Lecture 10, Part A - Definition and History of Lambert's Problem
26 AEE462 Lecture 10, Part B - Lambert's Equation and the Solution to Lambert's Problem
27 AEE462 Lecture 10, Part C - A Bisection Algorithm for the Solution of Lambert's Equation
28 AEE462 Lecture11 - A Minicourse on Rocketry
29 AEE 462 Lecture 12 - Orbital Perturbations and Atmospheric Drag
30 AEE 462 Lecture 13 - The J2 Orbital Perturbation and Applications (corrected)
31 AEE 462 Lecture 14a - Sphere of Influence and Orbit of the Moon
32 AEE 462 Lecture 14b - Interplanetary Mission Planning (Venus Orbiter)
33 AEE462 lecture 14c - Gravitational Assist Maneuvers
34 AEE462 Lecture15a - Introduction to Spacecraft Design
35 AEE462 Lecture15b - Attitude Determination and Control Systems (ADCS)
36 AEE462 Lecture16a - Euler's Equations
37 AEE462 Lecture16b - Spacecract Precession and Nutation
38 AEE462 Lecture16b - Spacecract Precession and Nutation
39 AEE 462 Lecture 17c - A Demonstration of Minor Axis Instability
40 AEE 462 Lecture 17a - Spin Stability and the Intermediate Axis Theorem
41 AEE 462 Lecture 17b - Energy Dissipation and Spin Stability about the Minor Axis