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Main
Installation
Changelog
Bibliography
Tutorials
Basic
The various anomalies in pykep
Modified equinoctial elements in pykep
Epochs and Julian Dates
Planets and User Defined Planets (UDPLAs)
Interfacing to SPICE and JPL DE ephs
Lagrange Propagation
The Zero Hold simple sail dynamics
The CR3BP and BCP dynamics
Approximators for low-thrust transfers
The Sims-Flanagan trajectory leg
The Zero-Order-Hold trajectory leg
Plotting
Trajectory Optimization
Sims-Flanagan: point to point low-thrust transfer
Sims-Flanagan: planet to plane low-thrust transfer
Sims-Flanagan: planet to plane low-thrust transfer (with Alpha encoding)
Zero-Order Hold: TOPS problems I
Zero-Order Hold: TOPS problems II (free boundaries)
Multiple Gravity Assist (MGA)
Multiple Gravity Assist with one DSM (MGA-1DSM)
Multiple impulses: planet to planet transfer
Indirect methods I (minimum propellant, fixed time)
Indirect methods II (minimum time, Cartesian)
Indirect methods III (minimum propellant, fixed time, MEE)
Indirect methods IV (minimum time, MEE)
Primer Vector
Surrogate Primer Vector
API
Basic API
Anomalies Conversions
Global constants
Orbital Elements
Epoch class
Planet class
User defined planets (UDPLAs)
Lambert class
Fly-by routines
Various approximations for orbital transfers
Numerical Propagation
Interplanetary transfer legs
Trajectory Optimization
Trajectory Optimization Gym
The plot module
Utils
Repository
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