Index

A

a (AMAT.approach.Approach attribute) (AMAT.orbiter.Orbiter attribute) A (AMAT.vehicle.Vehicle attribute) a0 (AMAT.planet.Planet attribute) (AMAT.visibility.LanderToPlanet attribute) a_n() (AMAT.vehicle.Vehicle method) a_nbar() (AMAT.vehicle.Vehicle method) a_nvectorized() (AMAT.vehicle.Vehicle method) a_orbiter_defl (AMAT.orbiter.Orbiter attribute) a_probe_orbit (AMAT.orbiter.Orbiter attribute) a_s() (AMAT.vehicle.Vehicle method) a_sbar() (AMAT.vehicle.Vehicle method) a_svectorized() (AMAT.vehicle.Vehicle method) a_w() (AMAT.vehicle.Vehicle method) a_wbar() (AMAT.vehicle.Vehicle method) a_wvectorized() (AMAT.vehicle.Vehicle method) Abar (AMAT.vehicle.Vehicle attribute) acc_drag_array (AMAT.vehicle.Vehicle attribute) acc_drag_g (AMAT.vehicle.Vehicle attribute) acc_net_g (AMAT.vehicle.Vehicle attribute) acc_net_g_eg (AMAT.vehicle.Vehicle attribute) acc_net_g_en (AMAT.vehicle.Vehicle attribute) acc_net_g_full (AMAT.vehicle.Vehicle attribute) acc_step_array (AMAT.vehicle.Vehicle attribute) alpha (AMAT.vehicle.Vehicle attribute) AMAT.approach module AMAT.arrival module AMAT.interplanetary module

AMAT.launcher module AMAT.maneuver module AMAT.orbiter module AMAT.planet module AMAT.telecom module AMAT.vehicle module AMAT.visibility module angle (AMAT.arrival.Arrival attribute) Approach (class in AMAT.approach) Ar (AMAT.telecom.Link attribute) Arrival (class in AMAT.arrival) arrival_date (AMAT.visibility.LanderToPlanet attribute) At (AMAT.telecom.Link attribute) ATM (AMAT.planet.Planet attribute) ATM_density (AMAT.planet.Planet attribute) ATM_height (AMAT.planet.Planet attribute) ATM_pressure (AMAT.planet.Planet attribute) atm_probe_entry_local_latitude_parallel_vec_unit (AMAT.orbiter.Orbiter attribute) ATM_sonic (AMAT.planet.Planet attribute) ATM_temp (AMAT.planet.Planet attribute) avectorized() (AMAT.planet.Planet method) Avinf (AMAT.interplanetary.Interplanetary attribute)

B

b_mag (AMAT.approach.Approach attribute) b_plane_angle_theta (AMAT.approach.Approach attribute) B_vec_bi (AMAT.approach.Approach attribute) B_vec_bi_unit (AMAT.approach.Approach attribute) beta (AMAT.approach.Approach attribute) (AMAT.vehicle.Vehicle attribute)

beta1 (AMAT.vehicle.Vehicle attribute) beta_array (AMAT.visibility.LanderToOrbiter attribute) (AMAT.visibility.LanderToPlanet attribute) betaRatio (AMAT.vehicle.Vehicle attribute) BI_to_BI_dprime() (AMAT.approach.Approach method)

C

C3 (AMAT.interplanetary.Interplanetary attribute) CD (AMAT.vehicle.Vehicle attribute) cfgammabar() (AMAT.vehicle.Vehicle method) cfpsibar() (AMAT.vehicle.Vehicle method) cfvbar() (AMAT.vehicle.Vehicle method) checkAtmProfiles() (AMAT.planet.Planet method) CL (AMAT.vehicle.Vehicle attribute) classifyTrajectory() (AMAT.vehicle.Vehicle method) cogammabar() (AMAT.vehicle.Vehicle method) compute_antenna_gain() (AMAT.telecom.Link method) compute_apoapsis_raise_DV() (AMAT.vehicle.Vehicle method) compute_ApoapsisAltitudeKm() (AMAT.vehicle.Vehicle method) compute_coast_orbital_elements() (AMAT.orbiter.Orbiter method) compute_coast_trajectory() (AMAT.orbiter.Orbiter method) compute_data_volume() (AMAT.telecom.Link method) compute_dB() (AMAT.telecom.Link method) compute_declination() (AMAT.arrival.Arrival method) compute_exit_state_atm_relative() (AMAT.orbiter.Orbiter method) compute_exit_state_inertial() (AMAT.orbiter.Orbiter method) compute_free_space_loss_dB() (AMAT.telecom.Link method) compute_launch_capability() (AMAT.interplanetary.Interplanetary method) compute_orbit_trajectory() (AMAT.orbiter.Orbiter method) (AMAT.orbiter.PropulsiveOrbiter method) compute_orbiter_deflection_trajectory() (AMAT.orbiter.Orbiter method) compute_periapsis_raise_DV() (AMAT.vehicle.Vehicle method) compute_PeriapsisAltitudeKm() (AMAT.vehicle.Vehicle method) compute_post_PRM_orbital_elements() (AMAT.orbiter.Orbiter method) compute_PRM_dv() (AMAT.orbiter.Orbiter method) compute_probe_targeting_trajectory() (AMAT.orbiter.Orbiter method)

compute_timed_orbit_trajectory() (AMAT.orbiter.PropulsiveOrbiter method) compute_v_inf_mag() (AMAT.arrival.Arrival method) compute_v_inf_vector() (AMAT.arrival.Arrival method) computeAccelerationDrag() (AMAT.vehicle.Vehicle method) computeAccelerationLoad() (AMAT.vehicle.Vehicle method) computeAngMomScalar() (AMAT.vehicle.Vehicle method) computeDynPres() (AMAT.vehicle.Vehicle method) computeEccScalar() (AMAT.vehicle.Vehicle method) computeEnergy() (AMAT.vehicle.Vehicle method) computeEnergyScalar() (AMAT.vehicle.Vehicle method) computeH() (AMAT.planet.Planet method) computeHeatingForMultipleRN() (AMAT.vehicle.Vehicle method) computeMach() (AMAT.vehicle.Vehicle method) computeMachScalar() (AMAT.vehicle.Vehicle method) computeR() (AMAT.planet.Planet method) computeSemiMajorAxisScalar() (AMAT.vehicle.Vehicle method) computeStagPres() (AMAT.vehicle.Vehicle method) computeStagTemp() (AMAT.vehicle.Vehicle method) computeTCW() (AMAT.vehicle.Vehicle method) computeTCW2() (AMAT.vehicle.Vehicle method) computeTCWD() (AMAT.vehicle.Vehicle method) computeTCWD2() (AMAT.vehicle.Vehicle method) convertToKPa() (AMAT.vehicle.Vehicle method) convertToPerCm2() (AMAT.vehicle.Vehicle method) convertToPlotUnits() (AMAT.vehicle.Vehicle method) copsibar() (AMAT.vehicle.Vehicle method) CPCV (AMAT.planet.Planet attribute) createDensityMeasuredFunction() (AMAT.vehicle.Vehicle method) createQPlot() (AMAT.vehicle.Vehicle method)

D

D() (AMAT.vehicle.Vehicle method) d0 (AMAT.planet.Planet attribute) (AMAT.visibility.LanderToPlanet attribute) datafile (AMAT.interplanetary.Interplanetary attribute) (AMAT.launcher.Launcher attribute) Dbar() (AMAT.vehicle.Vehicle method) declination (AMAT.arrival.Arrival attribute) delta_deg_array (AMAT.vehicle.Vehicle attribute) delta_theta_star_probe (AMAT.maneuver.ProbeOrbiterDeflection attribute) delta_theta_star_probe1 (AMAT.maneuver.ProbeProbeDeflection attribute) delta_theta_star_probe2 (AMAT.maneuver.ProbeProbeDeflection attribute) delta_theta_star_space (AMAT.maneuver.ProbeOrbiterDeflection attribute) delta_theta_star_space1 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) delta_theta_star_space2 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) densAvgCol (AMAT.vehicle.Vehicle attribute) densHighCol (AMAT.vehicle.Vehicle attribute) density() (AMAT.planet.Planet method) density_int (AMAT.planet.Planet attribute) density_mes_array (AMAT.vehicle.Vehicle attribute) density_mes_int (AMAT.vehicle.Vehicle attribute) densityvectorized() (AMAT.planet.Planet method) densLowCol (AMAT.vehicle.Vehicle attribute)

densTotalCol (AMAT.vehicle.Vehicle attribute) df (AMAT.interplanetary.Interplanetary attribute) dimensionalize() (AMAT.planet.Planet method) Dr (AMAT.telecom.Link attribute) drange0_km (AMAT.vehicle.Vehicle attribute) drange_km_eg (AMAT.vehicle.Vehicle attribute) drange_km_en (AMAT.vehicle.Vehicle attribute) drange_km_full (AMAT.vehicle.Vehicle attribute) drange_kmc (AMAT.vehicle.Vehicle attribute) drangec (AMAT.vehicle.Vehicle attribute) Dt (AMAT.telecom.Link attribute) dt (AMAT.vehicle.Vehicle attribute) dummyVehicle() (AMAT.vehicle.Vehicle method) dV_mag_orbiter_defl (AMAT.orbiter.Orbiter attribute) dV_mag_probe_targeting (AMAT.orbiter.Orbiter attribute) dV_vec_orbiter_defl (AMAT.orbiter.Orbiter attribute) dV_vec_probe_targeting (AMAT.orbiter.Orbiter attribute) Dvectorized() (AMAT.vehicle.Vehicle method) dyn_pres_atm (AMAT.vehicle.Vehicle attribute) dyn_pres_atm_eg (AMAT.vehicle.Vehicle attribute) dyn_pres_atm_en (AMAT.vehicle.Vehicle attribute) dyn_pres_atm_full (AMAT.vehicle.Vehicle attribute)

E

e (AMAT.approach.Approach attribute) (AMAT.orbiter.Orbiter attribute) e_orbiter_defl (AMAT.orbiter.Orbiter attribute) e_probe_orbit (AMAT.orbiter.Orbiter attribute) e_vec_bi (AMAT.approach.Approach attribute) e_vec_bi_unit (AMAT.approach.Approach attribute) EARTHG (AMAT.planet.Planet attribute) EB_N0 (AMAT.telecom.Link attribute) EB_N0_margin (AMAT.telecom.Link attribute)

EB_N0_req (AMAT.telecom.Link attribute) EFPA_1sigma_value (AMAT.vehicle.Vehicle attribute) elevation_array (AMAT.visibility.LanderToOrbiter attribute) (AMAT.visibility.LanderToPlanet attribute) EOM() (AMAT.vehicle.Vehicle method) EOM2() (AMAT.vehicle.Vehicle method) eta_r (AMAT.telecom.Link attribute) eta_t (AMAT.telecom.Link attribute) exitflag (AMAT.vehicle.Vehicle attribute)

F

f (AMAT.launcher.Launcher attribute) findEFPALimitD() (AMAT.vehicle.Vehicle method) findEFPALimitD2() (AMAT.vehicle.Vehicle method) findOverShootLimit() (AMAT.vehicle.Vehicle method) findOverShootLimit2() (AMAT.vehicle.Vehicle method) findOverShootLimitD() (AMAT.vehicle.Vehicle method)

findOverShootLimitD2() (AMAT.vehicle.Vehicle method) findUnderShootLimit() (AMAT.vehicle.Vehicle method) findUnderShootLimit2() (AMAT.vehicle.Vehicle method) findUnderShootLimitD() (AMAT.vehicle.Vehicle method) findUnderShootLimitD2() (AMAT.vehicle.Vehicle method) freq (AMAT.telecom.Link attribute)

G

gamma0_deg (AMAT.vehicle.Vehicle attribute) gamma_atm_probe_entry (AMAT.orbiter.Orbiter attribute) gamma_deg_eg (AMAT.vehicle.Vehicle attribute) gamma_deg_en (AMAT.vehicle.Vehicle attribute) gamma_deg_full (AMAT.vehicle.Vehicle attribute) gamma_degc (AMAT.vehicle.Vehicle attribute) gamma_entry_atm (AMAT.approach.Approach attribute) gamma_entry_inertial (AMAT.approach.Approach attribute) gamma_entry_inertial_check (AMAT.approach.Approach attribute) gamma_inertial_probe_entry (AMAT.orbiter.Orbiter attribute) gammac (AMAT.vehicle.Vehicle attribute)

Ghdot (AMAT.vehicle.Vehicle attribute) GM (AMAT.planet.Planet attribute) gnbar() (AMAT.vehicle.Vehicle method) gphibar() (AMAT.vehicle.Vehicle method) Gq (AMAT.vehicle.Vehicle attribute) Gr_dBi (AMAT.telecom.Link attribute) grbar() (AMAT.vehicle.Vehicle method) gsbar() (AMAT.vehicle.Vehicle method) Gt_dBi (AMAT.telecom.Link attribute) gthetabar() (AMAT.vehicle.Vehicle method) gwbar() (AMAT.vehicle.Vehicle method)

H

h (AMAT.approach.Approach attribute) (AMAT.orbiter.Orbiter attribute) h0_km (AMAT.vehicle.Vehicle attribute) h_EI (AMAT.orbiter.Orbiter attribute) h_km_eg (AMAT.vehicle.Vehicle attribute) h_km_en (AMAT.vehicle.Vehicle attribute) h_km_full (AMAT.vehicle.Vehicle attribute) h_kmc (AMAT.vehicle.Vehicle attribute) h_low (AMAT.planet.Planet attribute) h_orbiter_defl (AMAT.orbiter.Orbiter attribute) h_periapsis_orbiter_defl (AMAT.orbiter.Orbiter attribute) h_periapsis_probe (AMAT.orbiter.Orbiter attribute) h_probe_orbit (AMAT.orbiter.Orbiter attribute) h_skip (AMAT.planet.Planet attribute) h_step_array (AMAT.vehicle.Vehicle attribute) h_switch (AMAT.vehicle.Vehicle attribute) h_thres (AMAT.planet.Planet attribute)

h_trap (AMAT.planet.Planet attribute) h_vec_bi (AMAT.approach.Approach attribute) h_vec_bi_unit (AMAT.approach.Approach attribute) hddot_array (AMAT.vehicle.Vehicle attribute) hdot_array (AMAT.vehicle.Vehicle attribute) hdot_threshold (AMAT.vehicle.Vehicle attribute) heading_atm_probe_entry (AMAT.orbiter.Orbiter attribute) heading_entry_atm (AMAT.approach.Approach attribute) heatload (AMAT.vehicle.Vehicle attribute) heatLoad0 (AMAT.vehicle.Vehicle attribute) heatload_eg (AMAT.vehicle.Vehicle attribute) heatload_en (AMAT.vehicle.Vehicle attribute) heatload_full (AMAT.vehicle.Vehicle attribute) heightCol (AMAT.vehicle.Vehicle attribute) heightInKmFlag (AMAT.vehicle.Vehicle attribute) hitsTargetApoapsis() (AMAT.vehicle.Vehicle method) hitsTargetApoapsis2() (AMAT.vehicle.Vehicle method)

I

i (AMAT.approach.Approach attribute) (AMAT.orbiter.Orbiter attribute) i_orbiter_defl (AMAT.orbiter.Orbiter attribute) i_probe_orbit (AMAT.orbiter.Orbiter attribute) ICRF_to_BI() (AMAT.approach.Approach method) (AMAT.visibility.Visibility method)

ID (AMAT.interplanetary.Interplanetary attribute) (AMAT.planet.Planet attribute) index (AMAT.vehicle.Vehicle attribute) Interplanetary (class in AMAT.interplanetary) isCaptured() (AMAT.vehicle.Vehicle method)

J

J2 (AMAT.planet.Planet attribute)

J3 (AMAT.planet.Planet attribute)

K

Ka_dB (AMAT.telecom.Link attribute)

kind (AMAT.launcher.Launcher attribute)

L

L() (AMAT.vehicle.Vehicle method) L_DSN_dB (AMAT.telecom.Link attribute) L_other_dB (AMAT.telecom.Link attribute) L_sc_dB (AMAT.telecom.Link attribute) La_dB (AMAT.telecom.Link attribute) lander_pos_x_bi_arr (AMAT.visibility.LanderToOrbiter attribute) lander_pos_y_bi_arr (AMAT.visibility.LanderToOrbiter attribute) lander_pos_z_bi_arr (AMAT.visibility.LanderToOrbiter attribute) LanderToOrbiter (class in AMAT.visibility) LanderToPlanet (class in AMAT.visibility) latitude_entry_bi (AMAT.approach.Approach attribute) latitude_probe_entry_bi (AMAT.orbiter.Orbiter attribute) Launcher (class in AMAT.launcher) launcherID (AMAT.launcher.Launcher attribute) launchMass() (AMAT.launcher.Launcher method) Lbar() (AMAT.vehicle.Vehicle method) Lcdate (AMAT.interplanetary.Interplanetary attribute)

LD (AMAT.vehicle.Vehicle attribute) LD_1sigma_value (AMAT.vehicle.Vehicle attribute) Link (class in AMAT.telecom) loadAtmosphereModel() (AMAT.planet.Planet method) loadAtmosphereModel5() (AMAT.planet.Planet method) loadAtmosphereModel6() (AMAT.planet.Planet method) loadMonteCarloDensityFile2() (AMAT.planet.Planet method) loadMonteCarloDensityFile3() (AMAT.planet.Planet method) local_latitude_parallel_vec_unit (AMAT.approach.Approach attribute) longitude_array (AMAT.visibility.LanderToOrbiter attribute) (AMAT.visibility.LanderToPlanet attribute) longitude_entry_bi (AMAT.approach.Approach attribute) longitude_probe_entry_bi (AMAT.orbiter.Orbiter attribute) longitude_rate (AMAT.visibility.LanderToOrbiter attribute) lowAlt_km (AMAT.vehicle.Vehicle attribute) Ls_dB (AMAT.telecom.Link attribute) Lt_dB (AMAT.telecom.Link attribute) Lvectorized() (AMAT.vehicle.Vehicle method)

M

makeBasicEntryPlots() (AMAT.vehicle.Vehicle method) mass (AMAT.vehicle.Vehicle attribute) maxRollRate (AMAT.vehicle.Vehicle attribute) maxTimeSecs (AMAT.vehicle.Vehicle attribute) mbar (AMAT.vehicle.Vehicle attribute) minAlt (AMAT.vehicle.Vehicle attribute) module AMAT.approach AMAT.arrival AMAT.interplanetary AMAT.launcher AMAT.maneuver AMAT.orbiter AMAT.planet AMAT.telecom AMAT.vehicle AMAT.visibility

N

N_ref_bi (AMAT.approach.Approach attribute) N_vec_bi (AMAT.approach.Approach attribute) N_vec_bi_unit (AMAT.approach.Approach attribute) NMONTE (AMAT.vehicle.Vehicle attribute) nominalEFPA (AMAT.vehicle.Vehicle attribute)

nominalLD (AMAT.vehicle.Vehicle attribute) nonDimState() (AMAT.planet.Planet method) north_pole (AMAT.arrival.Arrival attribute) NPOS (AMAT.vehicle.Vehicle attribute) nSigmaFunc() (AMAT.planet.Planet method) numPoints_lowAlt (AMAT.vehicle.Vehicle attribute)

O

obs_tar_pos_vec_bi_unit (AMAT.visibility.OrbiterToPlanet attribute) observer_planet (AMAT.visibility.LanderToPlanet attribute) OMEGA (AMAT.approach.Approach attribute) omega (AMAT.approach.Approach attribute) OMEGA (AMAT.orbiter.Orbiter attribute) omega (AMAT.orbiter.Orbiter attribute) OMEGA (AMAT.planet.Planet attribute) OMEGA_orbiter_defl (AMAT.orbiter.Orbiter attribute) omega_orbiter_defl (AMAT.orbiter.Orbiter attribute)

OMEGA_probe_orbit (AMAT.orbiter.Orbiter attribute) omega_probe_orbit (AMAT.orbiter.Orbiter attribute) OMEGAbar (AMAT.planet.Planet attribute) Orbiter (class in AMAT.orbiter) orbiter_pos_x_bi_arr (AMAT.visibility.LanderToOrbiter attribute) orbiter_pos_y_bi_arr (AMAT.visibility.LanderToOrbiter attribute) orbiter_pos_z_bi_arr (AMAT.visibility.LanderToOrbiter attribute) OrbiterOrbiterDeflection (class in AMAT.maneuver) OrbiterToPlanet (class in AMAT.visibility)

P

p_switch (AMAT.vehicle.Vehicle attribute) peri_alt_km (AMAT.orbiter.Orbiter attribute) phi0_deg (AMAT.vehicle.Vehicle attribute) phi_1 (AMAT.approach.Approach attribute) phi_2 (AMAT.approach.Approach attribute) phi_deg_eg (AMAT.vehicle.Vehicle attribute) phi_deg_en (AMAT.vehicle.Vehicle attribute) phi_deg_full (AMAT.vehicle.Vehicle attribute) phi_degc (AMAT.vehicle.Vehicle attribute) phic (AMAT.vehicle.Vehicle attribute) Planet (class in AMAT.planet) planetObj (AMAT.approach.Approach attribute) (AMAT.maneuver.OrbiterOrbiterDeflection attribute) (AMAT.maneuver.ProbeOrbiterDeflection attribute) (AMAT.maneuver.ProbeProbeDeflection attribute) (AMAT.vehicle.Vehicle attribute) (AMAT.visibility.LanderToPlanet attribute) plot_Avinf_vs_launch_date() (AMAT.interplanetary.Interplanetary method) plot_Avinf_vs_launch_date_with_launch_mass_colorbar() (AMAT.interplanetary.Interplanetary method) plot_launch_mass_vs_launch_date() (AMAT.interplanetary.Interplanetary method) plot_launch_mass_vs_TOF() (AMAT.interplanetary.Interplanetary method) plot_launch_mass_vs_TOF_with_vinf_colorbar() (AMAT.interplanetary.Interplanetary method) plot_TOF_vs_launch_date() (AMAT.interplanetary.Interplanetary method) pos_vec_bi() (AMAT.approach.Approach method) (AMAT.orbiter.Orbiter method) (AMAT.orbiter.PropulsiveOrbiter method) pos_vec_bi_dprime() (AMAT.approach.Approach method) pos_vec_bi_orbiter_defl() (AMAT.orbiter.Orbiter method) pos_vec_bi_probe() (AMAT.orbiter.Orbiter method) predictApoapsisAltitudeKm_afterJettision() (AMAT.vehicle.Vehicle method) predictApoapsisAltitudeKm_afterJettision2() (AMAT.vehicle.Vehicle method) predictApoapsisAltitudeKm_withLiftUp() (AMAT.vehicle.Vehicle method) predictApoapsisAltitudeKm_withLiftUp2() (AMAT.vehicle.Vehicle method) pressure_int (AMAT.planet.Planet attribute) pressurevectorized() (AMAT.planet.Planet method) presvectorized() (AMAT.planet.Planet method)

PRM_dv_mag (AMAT.orbiter.Orbiter attribute) PRM_dv_vec (AMAT.orbiter.Orbiter attribute) probe (AMAT.maneuver.ProbeOrbiterDeflection attribute) probe1 (AMAT.maneuver.ProbeProbeDeflection attribute) probe2 (AMAT.maneuver.ProbeProbeDeflection attribute) ProbeOrbiterDeflection (class in AMAT.maneuver) ProbeProbeDeflection (class in AMAT.maneuver) propogateEntry() (AMAT.vehicle.Vehicle method) propogateEntry2() (AMAT.vehicle.Vehicle method) propogateEntry_util() (AMAT.vehicle.Vehicle method) propogateEntry_util2() (AMAT.vehicle.Vehicle method) propogateEntry_utilD() (AMAT.vehicle.Vehicle method) propogateEntry_utilD2() (AMAT.vehicle.Vehicle method) propogateEntryPhaseD() (AMAT.vehicle.Vehicle method) propogateEntryPhaseD2() (AMAT.vehicle.Vehicle method) propogateEquilibriumGlide() (AMAT.vehicle.Vehicle method) propogateEquilibriumGlide2() (AMAT.vehicle.Vehicle method) propogateExitPhase() (AMAT.vehicle.Vehicle method) propogateExitPhase2() (AMAT.vehicle.Vehicle method) propogateExitPhaseD() (AMAT.vehicle.Vehicle method) propogateExitPhaseD2() (AMAT.vehicle.Vehicle method) propogateGuidedEntry() (AMAT.vehicle.Vehicle method) propogateGuidedEntry2() (AMAT.vehicle.Vehicle method) propogateGuidedEntryD() (AMAT.vehicle.Vehicle method) propogateGuidedEntryD2() (AMAT.vehicle.Vehicle method) PropulsiveOrbiter (class in AMAT.orbiter) psi0_deg (AMAT.vehicle.Vehicle attribute) psi_deg_eg (AMAT.vehicle.Vehicle attribute) psi_deg_en (AMAT.vehicle.Vehicle attribute) psi_deg_full (AMAT.vehicle.Vehicle attribute) psi_degc (AMAT.vehicle.Vehicle attribute) psic (AMAT.vehicle.Vehicle attribute) pSigmaFunc() (AMAT.planet.Planet method) psuedoController() (AMAT.vehicle.Vehicle method) Pt (AMAT.telecom.Link attribute) Pt_dB (AMAT.telecom.Link attribute)

Q

q_array (AMAT.vehicle.Vehicle attribute) q_stag_con (AMAT.vehicle.Vehicle attribute) q_stag_rad (AMAT.vehicle.Vehicle attribute) q_stag_total (AMAT.vehicle.Vehicle attribute) q_stag_total_eg (AMAT.vehicle.Vehicle attribute)

q_stag_total_en (AMAT.vehicle.Vehicle attribute) q_stag_total_full (AMAT.vehicle.Vehicle attribute) qref_array (AMAT.vehicle.Vehicle attribute) qStagConvective() (AMAT.vehicle.Vehicle method) qStagRadiative() (AMAT.vehicle.Vehicle method) qStagTotal() (AMAT.vehicle.Vehicle method)

R

R (AMAT.telecom.Link attribute) R1() (AMAT.approach.Approach method) (AMAT.visibility.Visibility method) R2() (AMAT.approach.Approach method) (AMAT.visibility.Visibility method) R3() (AMAT.approach.Approach method) (AMAT.visibility.Visibility method) r_apoapsis_mag (AMAT.orbiter.Orbiter attribute) r_apoapsis_orbiter_defl (AMAT.orbiter.Orbiter attribute) r_apoapsis_probe (AMAT.orbiter.Orbiter attribute) r_apoapsis_vec (AMAT.orbiter.Orbiter attribute) R_dBHz (AMAT.telecom.Link attribute) r_dv (AMAT.maneuver.OrbiterOrbiterDeflection attribute) (AMAT.maneuver.ProbeOrbiterDeflection attribute) (AMAT.maneuver.ProbeProbeDeflection attribute) r_dv_rp (AMAT.maneuver.OrbiterOrbiterDeflection attribute) (AMAT.maneuver.ProbeOrbiterDeflection attribute) (AMAT.maneuver.ProbeProbeDeflection attribute) r_EI (AMAT.approach.Approach attribute) (AMAT.orbiter.Orbiter attribute) r_mag_bi() (AMAT.approach.Approach method) (AMAT.orbiter.Orbiter method) (AMAT.orbiter.PropulsiveOrbiter method) r_periapsis_mag (AMAT.orbiter.Orbiter attribute) r_periapsis_orbiter_defl (AMAT.orbiter.Orbiter attribute) r_periapsis_probe (AMAT.orbiter.Orbiter attribute) R_vec_bi (AMAT.approach.Approach attribute) r_vec_bi_probe_entry (AMAT.orbiter.Orbiter attribute) r_vec_bi_probe_entry_mag (AMAT.orbiter.Orbiter attribute)

r_vec_bi_probe_entry_unit (AMAT.orbiter.Orbiter attribute) R_vec_bi_unit (AMAT.approach.Approach attribute) r_vec_dv (AMAT.maneuver.OrbiterOrbiterDeflection attribute) (AMAT.maneuver.ProbeOrbiterDeflection attribute) r_vec_dv_unit (AMAT.maneuver.OrbiterOrbiterDeflection attribute) (AMAT.maneuver.ProbeOrbiterDeflection attribute) r_vec_entry_bi (AMAT.approach.Approach attribute) r_vec_entry_bi_mag (AMAT.approach.Approach attribute) r_vec_entry_bi_unit (AMAT.approach.Approach attribute) range (AMAT.telecom.Link attribute) (AMAT.visibility.LanderToPlanet attribute) (AMAT.visibility.OrbiterToPlanet attribute) range_array (AMAT.visibility.LanderToOrbiter attribute) rbar() (AMAT.planet.Planet method) rc (AMAT.vehicle.Vehicle attribute) rho() (AMAT.planet.Planet method) rho0 (AMAT.planet.Planet attribute) rho2() (AMAT.planet.Planet method) rhobar() (AMAT.planet.Planet method) rhovectorized() (AMAT.planet.Planet method) RN (AMAT.vehicle.Vehicle attribute) RP (AMAT.planet.Planet attribute) rp_vec_bi (AMAT.approach.Approach attribute) rp_vec_bi_unit (AMAT.approach.Approach attribute) runMonteCarlo() (AMAT.vehicle.Vehicle method) runMonteCarlo2() (AMAT.vehicle.Vehicle method) runMonteCarloD() (AMAT.vehicle.Vehicle method) runMonteCarloD2() (AMAT.vehicle.Vehicle method) runMonteCarloD_Earth() (AMAT.vehicle.Vehicle method)

S

S_vec_bi (AMAT.approach.Approach attribute) S_vec_bi_unit (AMAT.approach.Approach attribute) scaleHeight() (AMAT.planet.Planet method) set_vinf_vec_from_lambert_arc() (AMAT.arrival.Arrival method) set_vinf_vec_manually() (AMAT.arrival.Arrival method) setCDMachFunction() (AMAT.vehicle.Vehicle method) setDragEntryPhaseParams() (AMAT.vehicle.Vehicle method) setDragModulationVehicleParams() (AMAT.vehicle.Vehicle method) setEquilibriumGlideParams() (AMAT.vehicle.Vehicle method) setInitialState() (AMAT.vehicle.Vehicle method) setMaxRollRate() (AMAT.vehicle.Vehicle method) setSolverParams() (AMAT.vehicle.Vehicle method) setTargetOrbitParams() (AMAT.vehicle.Vehicle method) setupMonteCarloSimulation() (AMAT.vehicle.Vehicle method)

setupMonteCarloSimulationD() (AMAT.vehicle.Vehicle method) setupMonteCarloSimulationD_Earth() (AMAT.vehicle.Vehicle method) sheet_name (AMAT.interplanetary.Interplanetary attribute) solveTrajectory() (AMAT.vehicle.Vehicle method) solveTrajectory2() (AMAT.vehicle.Vehicle method) sonic_int (AMAT.planet.Planet attribute) sonicvectorized() (AMAT.planet.Planet method) space (AMAT.maneuver.ProbeOrbiterDeflection attribute) space1 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) space2 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) stag_pres_atm (AMAT.vehicle.Vehicle attribute) stag_pres_atm_eg (AMAT.vehicle.Vehicle attribute) stag_pres_atm_en (AMAT.vehicle.Vehicle attribute) stag_pres_atm_full (AMAT.vehicle.Vehicle attribute)

T

t_array (AMAT.visibility.LanderToOrbiter attribute) (AMAT.visibility.LanderToPlanet attribute) (AMAT.visibility.OrbiterToPlanet attribute) t_min_eg (AMAT.vehicle.Vehicle attribute) t_min_en (AMAT.vehicle.Vehicle attribute) t_min_full (AMAT.vehicle.Vehicle attribute) t_minc (AMAT.vehicle.Vehicle attribute) t_step_array (AMAT.vehicle.Vehicle attribute) t_switch (AMAT.vehicle.Vehicle attribute) T_vec_bi (AMAT.approach.Approach attribute) T_vec_bi_unit (AMAT.approach.Approach attribute) target_apo_km (AMAT.vehicle.Vehicle attribute) target_apo_km_tol (AMAT.vehicle.Vehicle attribute) target_peri_km (AMAT.vehicle.Vehicle attribute) target_planet (AMAT.visibility.LanderToPlanet attribute) tau (AMAT.planet.Planet attribute) tc (AMAT.vehicle.Vehicle attribute) temp_int (AMAT.planet.Planet attribute) temperaturevectorized() (AMAT.planet.Planet method) tempvectorized() (AMAT.planet.Planet method) terminal_E (AMAT.orbiter.Orbiter attribute) terminal_fpa_ie_deg (AMAT.orbiter.Orbiter attribute) terminal_fpa_ie_rad (AMAT.orbiter.Orbiter attribute) terminal_g (AMAT.orbiter.Orbiter attribute) terminal_g_bi (AMAT.orbiter.Orbiter attribute) terminal_h (AMAT.orbiter.Orbiter attribute) terminal_phi (AMAT.orbiter.Orbiter attribute) terminal_phi_bi (AMAT.orbiter.Orbiter attribute) terminal_psi (AMAT.orbiter.Orbiter attribute) terminal_psi_bi (AMAT.orbiter.Orbiter attribute) terminal_r (AMAT.orbiter.Orbiter attribute) terminal_r_bi (AMAT.orbiter.Orbiter attribute) terminal_r_hat_vec (AMAT.orbiter.Orbiter attribute), [1] terminal_r_vec (AMAT.orbiter.Orbiter attribute)

terminal_theta (AMAT.orbiter.Orbiter attribute) terminal_theta_bi (AMAT.orbiter.Orbiter attribute) terminal_v (AMAT.orbiter.Orbiter attribute) terminal_v_bi (AMAT.orbiter.Orbiter attribute) terminal_v_ie_hat_vec (AMAT.orbiter.Orbiter attribute) terminal_v_ie_vec (AMAT.orbiter.Orbiter attribute) terminal_v_vec (AMAT.orbiter.Orbiter attribute) theta0_deg (AMAT.vehicle.Vehicle attribute) theta_deg_eg (AMAT.vehicle.Vehicle attribute) theta_deg_en (AMAT.vehicle.Vehicle attribute) theta_deg_full (AMAT.vehicle.Vehicle attribute) theta_degc (AMAT.vehicle.Vehicle attribute) theta_star_dv_probe (AMAT.maneuver.ProbeOrbiterDeflection attribute) theta_star_dv_probe1 (AMAT.maneuver.ProbeProbeDeflection attribute) theta_star_dv_probe2 (AMAT.maneuver.ProbeProbeDeflection attribute) theta_star_dv_space1 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) theta_star_entry (AMAT.approach.Approach attribute) theta_star_exit (AMAT.orbiter.Orbiter attribute) theta_star_orbiter_defl (AMAT.orbiter.Orbiter attribute) theta_star_probe_entry (AMAT.orbiter.Orbiter attribute) theta_star_probe_targeting (AMAT.orbiter.Orbiter attribute) thetac (AMAT.vehicle.Vehicle attribute) timeStep (AMAT.vehicle.Vehicle attribute) TOF (AMAT.interplanetary.Interplanetary attribute) TOF_probe (AMAT.maneuver.ProbeOrbiterDeflection attribute) TOF_probe1 (AMAT.maneuver.ProbeProbeDeflection attribute) TOF_probe2 (AMAT.maneuver.ProbeProbeDeflection attribute) TOF_space (AMAT.maneuver.ProbeOrbiterDeflection attribute) TOF_space1 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) TOF_space2 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) tol (AMAT.vehicle.Vehicle attribute) truncateTrajectory() (AMAT.vehicle.Vehicle method) Ts (AMAT.telecom.Link attribute) Ts_dBK (AMAT.telecom.Link attribute)

U

userDefinedCDMach (AMAT.vehicle.Vehicle attribute)

V

v0_kms (AMAT.vehicle.Vehicle attribute) v_apoapsis_mag_coast (AMAT.orbiter.Orbiter attribute) v_apoapsis_mag_orbit (AMAT.orbiter.Orbiter attribute) v_apoapsis_vec_coast (AMAT.orbiter.Orbiter attribute) v_apoapsis_vec_orbit (AMAT.orbiter.Orbiter attribute) v_atm_probe_entry_unit_proj (AMAT.orbiter.Orbiter attribute) v_bi_mag_probe_entry (AMAT.orbiter.Orbiter attribute) v_bi_vec_probe_entry (AMAT.orbiter.Orbiter attribute) v_bi_vec_probe_entry_unit (AMAT.orbiter.Orbiter attribute) v_entry_atm_mag (AMAT.approach.Approach attribute) v_entry_inertial_mag (AMAT.approach.Approach attribute) v_inf_mag (AMAT.arrival.Arrival attribute) v_inf_vec (AMAT.arrival.Arrival attribute) v_inf_vec_bi (AMAT.approach.Approach attribute) v_inf_vec_bi_kms (AMAT.approach.Approach attribute) v_inf_vec_bi_mag_kms (AMAT.approach.Approach attribute) v_inf_vec_unit (AMAT.arrival.Arrival attribute) v_kms_eg (AMAT.vehicle.Vehicle attribute) v_kms_en (AMAT.vehicle.Vehicle attribute) v_kms_full (AMAT.vehicle.Vehicle attribute) v_kmsc (AMAT.vehicle.Vehicle attribute) v_mag_probe_entry_atm (AMAT.orbiter.Orbiter attribute) v_switch (AMAT.vehicle.Vehicle attribute) v_switch_kms (AMAT.vehicle.Vehicle attribute) v_vec_dv_maneuver (AMAT.maneuver.OrbiterOrbiterDeflection attribute) (AMAT.maneuver.ProbeOrbiterDeflection attribute) (AMAT.maneuver.ProbeProbeDeflection attribute) v_vec_dv_maneuver_mag (AMAT.maneuver.OrbiterOrbiterDeflection attribute) (AMAT.maneuver.ProbeOrbiterDeflection attribute) (AMAT.maneuver.ProbeProbeDeflection attribute)

v_vec_dv_probe (AMAT.maneuver.ProbeOrbiterDeflection attribute) v_vec_dv_probe1 (AMAT.maneuver.ProbeProbeDeflection attribute) v_vec_dv_probe2 (AMAT.maneuver.ProbeProbeDeflection attribute) v_vec_dv_space (AMAT.maneuver.ProbeOrbiterDeflection attribute) v_vec_dv_space1 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) v_vec_dv_space2 (AMAT.maneuver.OrbiterOrbiterDeflection attribute) v_vec_entry_atm (AMAT.approach.Approach attribute) v_vec_entry_atm_unit (AMAT.approach.Approach attribute) v_vec_entry_atm_unit_proj (AMAT.approach.Approach attribute) v_vec_entry_bi (AMAT.approach.Approach attribute) v_vec_entry_bi_unit (AMAT.approach.Approach attribute) v_vec_probe_entry_atm (AMAT.orbiter.Orbiter attribute) v_vec_probe_entry_atm_unit (AMAT.orbiter.Orbiter attribute) vc (AMAT.vehicle.Vehicle attribute) vehicle (AMAT.orbiter.Orbiter attribute) Vehicle (class in AMAT.vehicle) vehicleCopy (AMAT.vehicle.Vehicle attribute) vehicleID (AMAT.vehicle.Vehicle attribute) vel_vec_bi() (AMAT.approach.Approach method) (AMAT.orbiter.Orbiter method) (AMAT.orbiter.PropulsiveOrbiter method) vel_vec_bi_probe() (AMAT.orbiter.Orbiter method) vel_vec_entry_atm() (AMAT.approach.Approach method) vel_vec_probe_entry_atm() (AMAT.orbiter.Orbiter method) Visibility (class in AMAT.visibility) visible_array (AMAT.visibility.LanderToOrbiter attribute) (AMAT.visibility.LanderToPlanet attribute) (AMAT.visibility.OrbiterToPlanet attribute) Vref (AMAT.planet.Planet attribute)

W

wavelength (AMAT.telecom.Link attribute)

X

x_coast_arr (AMAT.orbiter.Orbiter attribute) x_orbit_arr (AMAT.orbiter.Orbiter attribute)

x_orbiter_defl_arr (AMAT.orbiter.Orbiter attribute) x_probe_arr (AMAT.orbiter.Orbiter attribute)

Y

y_coast_arr (AMAT.orbiter.Orbiter attribute) y_orbit_arr (AMAT.orbiter.Orbiter attribute)

y_orbiter_defl_arr (AMAT.orbiter.Orbiter attribute) y_probe_arr (AMAT.orbiter.Orbiter attribute)

Z

z_coast_arr (AMAT.orbiter.Orbiter attribute) z_orbit_arr (AMAT.orbiter.Orbiter attribute)

z_orbiter_defl_arr (AMAT.orbiter.Orbiter attribute) z_probe_arr (AMAT.orbiter.Orbiter attribute)