Index

A

Actuators (class in actuators) actuators (module) (spacecraft.Spacecraft attribute) add_noise() (actuators.Actuators method)

angular_velocity_derivative() (in module dynamics) apply_control_torques() (actuators.Actuators method) (spacecraft.Spacecraft method) approximate_gravity_gradient_torque() (spacecraft.Spacecraft method) approximate_magnetic_field_torque() (spacecraft.Spacecraft method)

B

bias (sensors.Gyros attribute)

C

C_w (actuators.Actuators attribute) calculate_attitude_error() (in module errors) calculate_attitude_rate_error() (in module errors) calculate_control_torques() (controller.PDController method) (spacecraft.Spacecraft method)

compute_earth_direction() (in module sensor_models) compute_local_magnetic_field() (in module sensor_models) controller (module) (spacecraft.Spacecraft attribute) cross() (in module math_utils)

D

dcm_to_quaternion() (in module math_utils) derivatives_func() (in module simulation)

dipole (spacecraft.Spacecraft attribute) dynamics (module)

E

EarthHorizonSensor (class in sensors) errors (module) estimate_angular_velocity() (sensors.Gyros method) (spacecraft.Spacecraft method)

estimate_attitude() (spacecraft.Spacecraft method) estimate_earth_direction() (sensors.EarthHorizonSensor method) estimate_magnetic_field() (sensors.Magnetometer method)

G

get_DCM_i2NED() (in module math_utils) get_noise() (sensors.EarthHorizonSensor method) (sensors.Gyros method) (sensors.Magnetometer method)

gravity_gradient_torque() (in module perturbations) Gyros (class in sensors) gyros (spacecraft.Spacecraft attribute)

J

J (spacecraft.Spacecraft attribute)

K

k_d (controller.PDController attribute)

k_p (controller.PDController attribute) kinematics (module)

M

magnetic_field_torque() (in module perturbations) Magnetometer (class in sensors)

main() (in module project) math_utils (module)

N

noise_vals (actuators.Actuators attribute) (sensors.EarthHorizonSensor attribute) (sensors.Gyros attribute) (sensors.Magnetometer attribute)

normalize() (in module math_utils)

P

PDController (class in controller)

perturbations (module) project (module)

Q

q (spacecraft.Spacecraft attribute) quaternion_derivative() (in module kinematics)

quaternion_multiply() (in module math_utils) quaternion_to_dcm() (in module math_utils)

R

r (spacecraft.Spacecraft attribute)

rxwl_max_momentum (actuators.Actuators attribute) rxwl_max_torque (actuators.Actuators attribute)

S

sensor_models (module) sensors (module) simulate() (in module project) simulate_adcs() (in module simulation)

simulate_estimation_and_control() (in module simulation) simulation (module) skew_symmetric() (in module math_utils) Spacecraft (class in spacecraft) spacecraft (module)

T

t1_matrix() (in module math_utils) t2_matrix() (in module math_utils)

t3_matrix() (in module math_utils) triad() (in module math_utils)

V

v (spacecraft.Spacecraft attribute)

W

w (spacecraft.Spacecraft attribute)

w_rxwls (actuators.Actuators attribute)