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This repository was archived by the owner on Aug 5, 2024. It is now read-only.

Features

Sylvain Guillet edited this page Mar 7, 2024 · 10 revisions

This framework provides the following features :

  • Work with JPL Spice kernels and stars
  • Export simulation to Cosmographia
  • PDS Archive management
    • Generate archive from object
    • Generate object from archive
    • Validate archive from Xml schemas
  • Spacecraft propagator
    • Geopotentials model (Earth only)
    • Simplified atmospheric model (Earth and Mars only)
    • Solar radiation pressure
    • N-body perturbation
    • Impulsive maneuvers
    • Fuel balance
  • Small body propagator
    • Geopotentials model (Earth only)
    • Simplified atmospheric model (Earth and Mars only)
    • Solar radiation pressure
    • N-body perturbation
  • Compute and convert orbital parameters
    • State vector
    • Two lines elements
    • Equinoctial
    • Keplerian elements
  • Compute and convert coordinates system
    • Equatorial
    • Horizontal
    • Planetodetic
    • Planetodentric
  • Frame transformation
    • ICRF / J2000
    • Ecliptic J2000
    • Ecliptic B1950
    • Galactic
    • B1950
    • FK4
    • Body fixed frames and ITRF93 (High accuracy earth fixed frame)
  • Configure spacecraft
    • Clock
    • Fuel tank
    • Engines
    • Instrument
  • Impulse maneuvers :
    • Apogee height
    • Perigee height
    • Plane alignment
    • Combined maneuver
    • Apsidal alignment
    • Phasing
  • Attitudes
    • Instrument pointing toward an object
    • Nadir
    • Zenith
    • Prograde
    • Retrograde
    • Zenith
  • Surface site on any celestial body
  • Evaluate launch opportunities
  • Use or convert different time referential (Calendar, Julian, seconds from J2000, TDB, UTC, Local)
  • Get celestial body information based on Naif kernels
  • Find time windows based on distance constraints from spacecraft, celestial body or ground site
  • Find time windows based on occultation constraints from spacecraft, celestial body or ground site
  • Find time windows based on coordinate constraints from spacecraft, celestial body or ground site
  • Find time windows based on illumination constraints from ground site.
  • Find time windows when an object is in instrument field of view.
  • Manipulate kernel files
  • Math tools
    • Vector
    • Matrix
    • Quaternion
    • Lagrange interpolation
  • Use the Framework through CLI (Command line interface)
    • Propagate small body and visualize it with Cosmographia
    • Sub observer point
    • Angular separation
    • Orientation
    • Orbital parameters converter
    • Frame converter
    • Time converter
    • Celestial body information
    • Find time windows from coordinate constraint
    • Find time windows from distance constraint
    • Find time windows from occultation constraint
    • Find time windows from field of view constraint
    • Find time windows from illumination constraint
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