const double mach_states[]
const double deployment_states[]
double optimalAngle(double sim_time_step, double altitude, double temperature, double velocity, double pressure, double current_delta, double tilt_angle, double target_apogee, double tolerance, const double mach_states[5], const double deployment_states[6], const double cd_table[30])
Calculates the optimal constant airbrake angle to reach a target apogee.