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AEE462 Lecture16a - Euler's Equations
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Orbital Mechanics and Spacecraft Dynamics
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- 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
