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This purpose of this wiki is to provide an overview of the EO-Sim project and documentation. It also keeps track of the high-level project goals, and tasks.
The purpose of EO-Sim is to provide satellite mission data useful in mission design and operations. The current status and planned revisions are described below.
Presently there are 3 packages (and corresponding repos):
InstruPy Produces functionality to model instruments, and produce expected data metrics given the target geometry and the instrument specifications.
OrbitPy Provides orbit-propagation, coverage (different types), line-of-sight ground-station contact, eclipse, pixel-projection (under-dev) calculations. The orbit propagation and coverage core functionality is provided by the C++ package propcov
.
EOSim GUI Provides a graphical user interface to set basic mission parameters, simulate and visualize 2d plots and animation with CesiumJS. This is based on Tkinter.
InstruPy Continue as is.
OrbitPy
- Disband the
propcov
package. - Switch to third-party orbit-propagation libraries (e.g., skyfield, GMAT) for high fidelity orbit propagation calculations. OrbitPy shall only provide a wrapper, which can produce propagation data at a standard format, for limited set of coordinate frames.
- Core coverage library would be provided through the
CoverageKinematics
library (under dev). OrbitPy shall provide an wrapper (which shall also function as the Earth coverage applications layer). (How about GNSS-R coverage?)
EOSim GUI
- Archive the EOSim GUI package.
- Start a new package called as
MissionEvaluator
, whose function is to provide evaluation of mission data (coverage metrics, revisit time, new proposed metrics, etc.) - Utilize the visualization scripts in the EOSim GUI (2d and animations based) to provide visualization of the mission data.
Compatibility with TAT-C/ NOS-T
- Start a new
SystemModelPy
library, which would contain the schemas for initialization of the various objects used in EO-Sim, such as Satellite, Orbit, etc. This would also be used by the D-SHIELD Planner. - Start using
pydantic
,typing
,uuid
,enum
andgeojson_pydantic
packages in a similar way to how it has been used in TAT-C (see theschemas.py
files). docs link and NOS-T
Increasing (propagation & coverage calculation) accuracy
- (Automated) Grab nearest available TLE, and use for orbit propagation
- Incorporation of SKyField propagators
- GNSS-R coverage calculations with elliptical Earth approximation
Coverage Kinematics Library
Earth Coverage applications layer (wrapper) of the Coverage Kinematics library (OrbitPy)