53#ifndef MODELS_SENSORS_ACCELEROMETER_H
54#define MODELS_SENSORS_ACCELEROMETER_H
141 SIGNAL(mount_alignment_mf, clockwerk::Quaternion, clockwerk::Quaternion({1.0, 0.0, 0.0, 0.0}))
145 SIGNAL(resolution,
double, 0.0)
150 SIGNAL(seed_value,
int, 0)
160 SIGNAL(operational_power_draw,
double, 0.0)
186 SIGNAL(output_time, clockwerk::Time, clockwerk::Time(0, 0))
207 SIGNAL(is_valid,
bool, false)
210 SIGNAL(current_power_draw,
double, 0.0)
230 int16
start()
override;
#define SIGNAL(NAME, TYPE, INITIAL_VALUE)
Definition appmacros.h:27
#define START_PARAMS
Definition appmacros.h:42
#define END_OUTPUTS
Definition appmacros.h:33
#define END_PARAMS
Definition appmacros.h:47
#define START_OUTPUTS
Definition appmacros.h:28
#define END_INPUTS
Definition appmacros.h:40
#define START_INPUTS
Definition appmacros.h:35
Standard vector class derived from Matrix.
Definition CartesianVector.hpp:39
Class defining a direction cosine matrix inherited from Matrix.
Definition DCM.h:69
Frame class definition.
Definition Frame.h:96
Latency model.
Definition LatencyUtil.hpp:41
#define CartesianVector3
Definition mathmacros.h:43
PlanetDefaults earth_wgs84
Definition planetdefaults.cpp:22
Class to propagate CR3BP dynamics in characteristic units.
Definition statistics.hpp:22
CartesianVector3 _previous_bias
Temporary variable to hold the bias vector at last function call.
Definition Accelerometer.h:246
int16 start() override
Class to execute logging.
SIGNAL(_mu, double, warpos::earth_wgs84.mu)
CartesianVector3 _perturbed_accel_no_grav
Definition Accelerometer.h:249
MarkovUncertaintyModel _sensor_noise_model
The bias and noise model for sensor output.
Definition Accelerometer.h:240
clockwerk::DCM _dcm_sf_root
A DCM relating our sensor frame to root.
Definition Accelerometer.h:252
Frame _sensor_frame
The sensor frame in which all measurements will be taken.
Definition Accelerometer.h:237
void _configureInternal()
Function to configure sensor – runs in all constructors.
warptwin::RateMonitor * rateMonitor()
Accessor for the internal rate monitor model.
Definition Accelerometer.h:224
int16 activate() override
_accel_output_struct _last_output
Temporary variable for the latest recorded output added to latency model and dummy output for steppin...
Definition Accelerometer.h:264
MODEL(Servo) public int16 deactivate() override
Model to simulate a servo's motion.
@ MODEL
Simplified dynamics model representing motion in the circular restricted 3 body problem.
Definition ImNode.h:31
CartesianVector3 _perturbed_accel
Temporary variable to hold the perturbed acceleration with and without gravity.
Definition Accelerometer.h:249
LatencyUtil< double > _latency_model
The latency model for servo angle output.
Definition Servo.h:116
MODEL(Accelerometer) public warptwin::MarkovUncertaintyModel * getNoiseModel()
Accessor for the internal noise model.
Definition Accelerometer.h:220
int16 execute() override
Function to check monitor input conditions and set trigger flag accordingly. Should be implemented in...
RateMonitor _rate_monitor
Rate monitor to control the rate at which the sensor runs.
Definition Accelerometer.h:243
clockwerk::CartesianVector< 3 > _in_deadzone
Temporary variable for checking if sensor is in deadzone. Each element of vector corresponds to an ax...
Definition Accelerometer.h:258
double _latency_return
Temporary value for the return of the latency value.
Definition Servo.h:122
CartesianVector3 _gravity__sensor
The gravity vector as represented in the sensor frame.
Definition Accelerometer.h:255
Accelerometer Model.
Definition Accelerometer.h:102
CartesianVector3 meas_accel_sf
Definition Accelerometer.h:103
_accel_output_struct()
Definition Accelerometer.h:108
_accel_output_struct(CartesianVector3 meas_accel_sf, CartesianVector3 meas_accel_sf_incl_grav, CartesianVector3 bias, bool is_valid)
Definition Accelerometer.h:114
CartesianVector3 meas_accel_sf_incl_grav
Definition Accelerometer.h:104
bool is_valid
Definition Accelerometer.h:106
CartesianVector3 bias
Definition Accelerometer.h:105