Module attitude 

Attitude control analysis for SOLAR LINE.

Analyzes pointing accuracy requirements, flip maneuver dynamics, and miss-distance sensitivity for brachistochrone trajectories.

Functions

accuracy_to_pointing_error_rad

Navigation accuracy as angular precision.

flip_angular_momentum

Angular momentum for a flip maneuver (kg·m²/s).

flip_angular_rate

Angular rate for a flip maneuver (rad/s).

flip_rcs_torque

RCS torque required for a flip maneuver (N·m).

gravity_gradient_torque

Gravity gradient torque on an elongated spacecraft (N·m).

miss_distance_km

Miss distance (km) from pointing error during a constant-thrust burn.

required_pointing_rad

Required pointing accuracy (radians) to achieve a given miss distance.

velocity_error_from_pointing

Pointing error from thrust vector misalignment over a burn.