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Space Vehicles and Orbital Dynamics
Engineering & Social Sciences Program
Madrid, Spain
Dates: mid Jan 2027 - late May 2027
Space Vehicles and Orbital Dynamics
OVERVIEW
CEA CAPA Partner Institution: Universidad Carlos III de Madrid
Location: Madrid, Spain
Primary Subject Area: Aerospace Engineering
Instruction in: English
Course Code: 14169
Transcript Source: Partner Institution
Course Details: Level 400
Recommended Semester Credits: 3
Contact Hours: 42
Prerequisites: Calculus I, Linear Algebra, Physics I, Programming, Calculus II, Mechanics Applied to Aerospace Engineering, Advanced Mathematics, Modeling in Aerospace Engineering, Mechanics of Flight I.
DESCRIPTION
1. Two body problem
Conservation laws
Conics and orbital elements
2. Kepler's equation
Formulation for the elliptic, parabolic, hyperbolic cases
Numerical solution
3. Orbital maneuvers
Fundamentals of spherical trigonometry
Hohmann, bielliptic transfers; plane change; phasing maneuvers, electric orbit raising
4. Preliminary orbit determination
Gibbs problem, Gauss problem
Lambert's problem
Porkchop diagrams
5. Perturbations
Special perturbation methods
General perturbation methods
Drag, solar radiation, third body
Geopotential and spherical harmonics
6. Interplanetary trajectories
Patched-conics method
Launch and B-Plane targeting
7. Relative motion and rendezvous
Clohessy-Wiltshire equations
8. Circular restricted three body problem
Derivation and normalization. Jacobi's energy integral
Lagrange libration points
Stability and trajectories near Lagrange points
9. Space vehicles: attitude dynamics
Quaternions. Free body attitude dynamics
Gravity gradient
10. Introduction to space missions and space systems
Application orbits, types of missions
Spacecraft subsystems
Conservation laws
Conics and orbital elements
2. Kepler's equation
Formulation for the elliptic, parabolic, hyperbolic cases
Numerical solution
3. Orbital maneuvers
Fundamentals of spherical trigonometry
Hohmann, bielliptic transfers; plane change; phasing maneuvers, electric orbit raising
4. Preliminary orbit determination
Gibbs problem, Gauss problem
Lambert's problem
Porkchop diagrams
5. Perturbations
Special perturbation methods
General perturbation methods
Drag, solar radiation, third body
Geopotential and spherical harmonics
6. Interplanetary trajectories
Patched-conics method
Launch and B-Plane targeting
7. Relative motion and rendezvous
Clohessy-Wiltshire equations
8. Circular restricted three body problem
Derivation and normalization. Jacobi's energy integral
Lagrange libration points
Stability and trajectories near Lagrange points
9. Space vehicles: attitude dynamics
Quaternions. Free body attitude dynamics
Gravity gradient
10. Introduction to space missions and space systems
Application orbits, types of missions
Spacecraft subsystems