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Spacecraft Models Package 2.0
Spacecraft Models for DSim
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MEMS IMU model. Outputs rate and acceleration. More...
#include <imu_mems.h>
Public Member Functions | |
| imu_mems (dsim_model_setup *setup) | |
| Constructor. | |
| ~imu_mems () | |
| Destructor. | |
| void | initialize_data () |
| Initialize outlets and output variables. | |
| void | initialization_complete () |
| Finish initialization. | |
| void | complete_timestep () |
| Computation done prior to numerical integration. | |
| void | initialize_timestep () |
| Computation done prior to numerical integration. | |
| void | rhs (double t, double jd) |
| Computation done during numerical integration. | |
Public Member Functions inherited from powered_hardware | |
| void * | describe_setup (void *ds) |
| Describe the setup variables. | |
| void | initialize_data () |
| Initialize outlets and output variables. | |
| void | initialization_complete () |
| Finish initialization. | |
| void | initialize_timestep () |
| Initialize the timestep. | |
Protected Attributes | |
| dsim_variable | bodyRate_dsim |
| Body rate input. | |
| dsim_variable | acceleration_dsim |
| Linear acceleration input. | |
| dsim_variable | angularAcceleration_dsim |
| Angular acceleration input. | |
| dsim_variable | centerOfMass_dsim |
| Linear acceleration input. | |
| dsim_variable | body_rate_measured_dsim |
| Measured body rate. | |
| dsim_variable | acceleration_measured_dsim |
| Linear acceleration input. | |
| dsim_variable | integratedRate_dsim |
| Angular rate input. | |
| dsim_variable | biasAccelerometer_dsim |
| Angular rate input. | |
| dsim_variable | biasGyro_dsim |
| Angular rate input. | |
| dsim_variable | imuPosition_dsim |
| Angular rate input. | |
| dsim_variable | imuBodyToIMUMatrix_dsim |
| Angular rate input. | |
| dsim_variable | oneSigmaGyroBias_dsim |
| Gyro random walk noise. | |
| dsim_variable | oneSigmaAccelerometerBias_dsim |
| Accelerometer random walk noise. | |
| dsim_variable | oneSigmaGyro_dsim |
| Gyro output noise. | |
| dsim_variable | oneSigmaAccelerometer_dsim |
| Accelerometer output noise. | |
| dsim_variable | tauGyroBias_dsim |
| Gyro bias time constant. | |
| dsim_variable | tauAccelerometerBias_dsim |
| Accelerometer bias time constant. | |
| dsim_variable | omegaConstant_dsim |
| Gyro constant rate. | |
| dsim_variable | accelerationConstant_dsim |
| Accelerometer constant rate. | |
| dsim_variable | imuBodyToIMUMatrix_param_dsim |
| Accelerometer constant rate. | |
| dsim_variable | imuPosition_param_dsim |
| Position constant. | |
Protected Attributes inherited from powered_hardware | |
| dsim_variable | power_on_dsim |
| Power consumed when on (constant) | |
| dsim_variable | power_standby_dsim |
| Power consumed when in standby mode (constant) | |
| dsim_variable | failed_dsim |
| Command flag for failed (1) or not (0) | |
| dsim_variable | on_dsim |
| Command flag for on (1) or off (1) | |
| dsim_variable | current_dsim |
| Measured current. | |
| dsim_variable | voltage_dsim |
| Input voltage. | |
| dsim_variable | thermal_node_dsim |
| Thermal node. | |
| dsim_variable | heat_dsim |
| Heat. | |
| dsim_variable | power_dsim |
| Power. | |
MEMS IMU model. Outputs rate and acceleration.
Models an inertial measurement unit with 3 orthogonal linear accelerometers and 3 rate gyros. The model for both gyro and accelerometer is
omega = omega_true + bias + constant + noise dbias/dt + bias/tau = noise
The second equation is for a Markov model. If tau = infinity this is a random walk model
Reference: Warren S. Flenniken IV, John H. Wall, David M. Bevly, "Characterization of Various IMU Error Sources and the Effect on Navigation Performance"