Spacecraft Models

Classes
class	oscillator
	Oscillator. More...
class	lunar_to_eci
	Convert planet orbiting initial conditions to heliocentric coordinates using spice. More...
class	lvlh_to_eci
	Convert LVLH initial conditions to ECI coordinates. More...
class	multi_body_hub
	Rigid body with multiple reaction wheels. More...
class	multi_body_hub_with_rwa
	Rigid body with multiple reaction wheels. More...
class	state_space_vehicle
	Continuous state space system. More...
class	po_to_helio
	Convert planet orbiting initial conditions to heliocentric coordinates using spice. More...
class	rigid_body
	Rigid body dynamical model applying both force and torque to the spacecraft. More...
class	rigid_body_no_rate_dynamics
	Rigid body dynamical model applying force and body rae to the spacecraft. More...
class	rigid_body_rwa
	Rigid body with multiple reaction wheels. More...

Detailed Description

These are the dynamical models for different types of spacecraft, including a basic rigid body, a rigid body with wheels, etc. There are also several utility models that allow the initial conditions (position/velocity, attitude) for the spacecraft to be defined in frames other than ECI.