Launch_Manager.py 文件源码

def insertion_pitch(self):
        _circ_dv = self.circ_dv()
        _t_ap_dv = self.target_apoapsis_speed_dv()
        _m = np.rad2deg(self.mean_anomaly())
        _burn_time = self.maneuver_burn_time(self.circ_dv())

        @jit(nopython=True)
        def pitch_calcs_low():
                return (_t_ap_dv * (_circ_dv / 1000)) + (_m - (180 - (_burn_time / 12)))

        @jit(nopython=True)
        def pitch_calcs_high():
                return (_t_ap_dv * (_circ_dv / 1000)) + (_m - 180)

        if self.parking_orbit_alt <= 300000: return pitch_calcs_low()
        else: return pitch_calcs_high()