Satellite-based Communication, Navigation & Surveillance

Space Flight Dynamics and Satellite Constellations

Objectives

Present an overview of the fundamentals of space flight dynamics. Mathematical principles will be explored for apprehending the physics of orbital motion, but they will be associated with descriptions of real implementations of space systems according to various mission requirements. The trainees will acquire a basic knowledge of the models describing trajectories and attitudes of space vehicles. They will also learn how to assess space related performances of a satellite based system. After completing this course you will be able to: understand the dynamics of the orbital motion, understand the complexity of the choice of a good time and reference system, select an orbit according to the main mission requirements, compute orbital manoeuvres for simple orbital transfers, select a satellite constellation or a formation flying system according to the mission performance requirements, understand the basic principles of space navigation systems.

Educational content

1. Fundamentals of Space Flight Dynamics

Kepler and Newton laws

2-body and 3-body problems

Orbital elements

Time and terrestrial reference systems

2. Orbital Perturbations

Modelling of the gravitational field

Detailed effect of the main zonal term (J2)

Sun and Moon and planets gravitational perturbations effects (illustrations with GPS orbits)

Sune radiations

Solar pressure

3. Orbital Manoeuvres

Impulsive manoeuvres

Modification of the orbital elements

Hohmann orbital transfer

Rendezvous

Station keeping

Deorbitation

4. Orbit Design

Main types of Earth orbits and basic properties

Earth-phased orbits

Geosynchronous orbits

Sunsynchronous orbits

Grounds tracks

5. Satellite Constellations

Constellation design

Visibility coverage

DOP coverage

Launch and deployment of satellite constellations

Station positioning strategies

Satellite renewal strategies

Examples of satellite constellations

6. Formation Flying Missions

Design of a formation flying system

Station keeping strategies

Examples of formation flying missions

7. Introduction to Satellite Navigation Systems

Previous navigation systems (TRANSIT, LORAN C)

Presentation of GPS, GLONASS and GALILEO

Principles of satellite positioning systems

Geometric dilution of precision (GDOP, PDOP, HDOP, VDOP, TDOP)

User equivalent range error (UERE)

For information only : 27 hours

Participates

Engineers and executives.
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