celestlab
Coordinates and frames >>
celestlab
>> - Introduction -
- Introduction -
Overview
Overview of CelestLab
—
Overview of CelestLab
Configuration
—
Configuration of CelestLab
CelestLab data
—
Overview of data available in CelestLab
Flight dynamics
Dates and time scales
—
Dates and time scales
Reference frames
—
Reference frames
Local frames
—
Local frames
Orbital elements
—
Description of orbital elements
Ephemerides for celestial bodies
—
Ephemerides for solar system bodies
Force models
—
Description of force models (acceleration and potential)
Orbit propagation models
—
Description of orbit propagation models available in CelestLab
STELA propagation model
—
Description of STELA (long-term) orbit propagation model
Two Line Elements
—
Two-Line Elements in CelestLab
Natural relative motion
—
Orbital elements and relative motion
Usage and conventions
Functions
—
Functions
Data types
—
Data types used in CelestLab
Flight dynamics conventions
—
Flight dynamics conventions
Cookbook
Frame transformations
—
Frame transformations
Numerical integration of orbital motion
—
Numerical integration
Rotations
—
Use of quaternions and frame transformation matrices
Simple orbital simulation
—
Calculation of classical orbital characteristics and events
Interplanetary cruise
—
Interplanetary trajectory calculation
Jacobian and covariance matrices
—
Jacobian and covariance matrices
Comparison of orbit propagation models
—
Comparison of propagation models
Basic orbit determination
—
Basic orbit determination, application to TLE estimation
Handling time scales
—
Time scales - best practices
B-plane
—
B-plane calculations
Calculation of atmospheric drag
—
Effect of atmospheric drag for a complex object
Report an issue
celestlab
Coordinates and frames >>