AE470: Orbital Mechanics at Clarkson University
- Slides: Week1
- Notebook: Setting Up the Environment
- Notebook: Prerequisite Material
- Notebook: Equations of Motion and Numerical Integration
- Notebook: Constants of Motion
- Notebook: Keplerian Orbits
- Notebook: Keplerian Orbits - Time of Flight
- Slides: Reference Frames
- Notebook: Rotation Matrices
- Slides: Classical Orbital Elements
- Notebook: Classical Orbital Elements
- Notebook: Time, Date, Ground Tracks
- Slides: Orbital Maneuvers 01
- Slides: Orbital Maneuvers 02
- Slides: Orbit Determination
- Slides: GPS
- Slides: Interplanetary Trajectories 01
- Slides: Interplanetary Trajectories 02
- Notebook: Interplanetary Trajectories
- Slides: Orbit Perturbations
- Notebook: Circular Restricted Three-Body Problem
- Assignment #1 - Numerical Integration
- Assignment #2 - Two-Body Problems
- Assignment #3 - Classical Orbital Elements
- Assignment #4 - Interplanetary Trajectories