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Spacecraft Models Package 2.0
Spacecraft Models for DSim
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| Caerodynamics_newtonian | Generates a Newtonian flow aerodynamic model using triangles |
| Canalog_sun_sensor | Provides a simple analog_sun_sensor model |
| Cbevel | A bevel or shim which provides a fixed rotation matrix between its parent and child |
| Ccam_planet | Cam_planet - used internally to maintain a list of planets present |
| Ccam_spacecraft | Cam_spacecraft - used internally to maintain a list of spacecraft present |
| Ccamera | Uses OpenGL to create synthetic camera images |
| Ccamera_context | A class used internally by the camera module |
| Ccomm_link | Geometric intersatellite link model based on S/N ratio |
| Ccomm_link_earth | Ground station contact model |
| Cdisturbances | Models solar pressure disturbances |
| Cdisturbances_earth | Generates a disturbance model for earth orbit |
| Cdisturbances_simple_earth | Generates a simple disturbance model for earth orbit |
| Cdouble_gimbal | A double_gimbal that accepts a rate command |
| Cearth_sensor_scanning | Provides a simple earth_sensor_scanning model |
| Celectric_thruster | Models a pulsewidth modulated suite of thrusters with a single blowdown tank |
| Cfusion_engine | A simple fusion engine model |
| Cgeometry_reader | Reads a geometry file giving one face per line and makes the data available as variables |
| Cgimbal | A single axis gimbal that accepts a rate command |
| Cgravity_earth_harmonics | Models the spherical harmonic gravity about a single planet |
| Cgravity_earth_ideal | A point gravity model |
| Cgravity_spice | SPICE library ephemeris interface class |
| Cgravity_spice_jupiter | SPICE library ephemeris interface class |
| Cgravity_two_solar_system | Generates gravity for two solar systems |
| Cground_station | Models an earth fixed ground station that can send messages |
| Chinge_motor | Models a set of reaction wheels |
| Cideal_actuator | Apply force and torques to the parent object |
| Cimager | Imager model that outputs centroids |
| Cimu | Rate integrating IMU model |
| Cinfrared_imager | Infrared imager model |
| Cisl | A simplified geometric intersatellite link model |
| Cisothermal | Isothermal spacecraft model |
| Cjupiter_moon_propagation | Compute the positions and velocities of the Galilean moons |
| Cload | An electrical and heat load model |
| Clunar_landing_sensors | Models lunar landering sensors |
| Clunar_surface_constraint | Provides constraint forces so an object stays fixed to the ground |
| Clunar_to_eci | Convert planet orbiting initial conditions to heliocentric coordinates using spice |
| Clvlh_to_eci | Convert LVLH initial conditions to ECI coordinates |
| Cmagnetic_field | Magnetic field using Earth dipole model |
| Cmagnetic_torquer | Magnetic torquer model |
| Cmagnetometer | 3-axis magnetometer model |
| Cmulti_body_hub | Rigid body with multiple reaction wheels |
| Cmulti_body_hub_with_rwa | Rigid body with multiple reaction wheels |
| Cnet_acceleration | Compute net acceleration including centripetal |
| Coscillator | Oscillator |
| Cphones | Computes the position of a user on the earth and determines if they are in range of a satellite |
| Cpo_to_helio | Convert planet orbiting initial conditions to heliocentric coordinates using spice |
| Cpower_system | A power system model |
| ▼Cpowered_hardware | A super class for powered hardware |
| Cantenna | An antenna beam model solely for display purposes |
| Cbattery | Models a battery |
| Cgps_receiver | Simplified geometric GPS receiver model |
| Cimu_mems | MEMS IMU model. Outputs rate and acceleration |
| Cstar_tracker | Provides a simple star_tracker model |
| Cpropulsion | Models a pulsewidth modulated suite of thrusters with a single blowdown tank |
| Cpropulsion_constant_thrust | Models a pulsewidth modulated suite of thrusters with a single blowdown tank |
| Cradiator | Models a simple communications link |
| Crate_and_force_actuator | A component used to allow a controller (or other component) to apply ideal forces and torques to the actuator's parent |
| Creaction_wheel | Models a set of reaction wheels |
| Creaction_wheel_bristle | Models a set of reaction wheels |
| Crigid_body | Rigid body dynamical model applying both force and torque to the spacecraft |
| Crigid_body_no_rate_dynamics | Rigid body dynamical model applying force and body rae to the spacecraft |
| Crigid_body_rwa | Rigid body with multiple reaction wheels |
| Crk78 | Verner's Runge Kutta 7/8 order variable step integrator |
| Crv_to_kepler | Converts position and velocity to Keplerian elements |
| ▼Csensor | Sensor base class |
| Chsa | Scanning horizon sensor model |
| Csingle_axis_sun_sensor | Implements a single axis sun sensor |
| Csolar_flux | Solar flux model using SPICE ephemeris |
| Csolar_panel | A solar panel model |
| Csolar_panel_rotating | A rotating solar panel model |
| Csolar_pressure | Generates a solar pressure model anywhere in the solar system but only in interplanetary space |
| Csolar_sail | Compute the solar force and torque on a thin membrane using a combined optical/thermal model |
| Cstar_camera | Star camera model that outputs centroids of planets and stars |
| Cstate_space_vehicle | Continuous state space system |
| Csun_sensor | A geometric sun sensor model |
| Csun_sensor_two_axis | Provides a simple sun_sensor_two_axis model |
| Csun_sensor_two_axis_array | Provides a simple sun_sensor_two_axis_array model |
| Ctarget_sensor | Target_sensor model that outputs relative state |
| Ctelescope_payload | Provides a simple telescope payload |
| Ctext_sender | Sends text messages |
| Cthermal | Provides a simple thermal model for a network of elements |
| Ctime_base | Time sensor to return Julian Day Number |
| Ctracking_station | Generates position and velocity of the target in the ECI frame |
| Cwarfighter | Provides a warfighter model |