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Define mission control sequence segments usin ... [more]
Define mission control sequence segments using pre-defined calculation objects
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Time duration; Epoch; Keplerian elements; Access; XYZ positi ... [more]
Time duration; Epoch; Keplerian elements; Access; XYZ position/velocity vectors; Delaunay G, H, L, and Semi-Latus Rectum; Equinoctial h, k, p, q and Mean Longitude; Maneuver delta V (integrated along orbit path), FuelMass, Fuel Density, Fuel Used, Inertial delta V Magnitude, Inertial delta Vx, Inertial delta Vy, Inertial delta Vz, Specific Impulse, Tank Pressure, Tank Temperature, Thrust Vector X, Thrust Vector Y, Thrust Vector Z, Total Mass and Total Mass Flow Rate; Beta angle, C3 energy and true longitude; Formation flying values; Atmospheric density, pressure and temperature; Geostationary longitude drift rate in angle/time; Geodetic latitude, longitude, altitude, height above terrain, longitude rate, altitude rate; Repeating Ground Track Error; Absolute Value, Difference, Maximum Value, Minimum Value, and Negative; Kozai-Izsak and Brouwer-Lyddane means; Multibody B-plane elements, delta declination and right ascension; Internal, Processed and Solar Array power; Motion relative to a reference satellite; Spacecraft Drag, Radiation Pressure, and Solar Radiation Pressure; Cosine of vertical FPA, declination, declination rate, flight path angle, R magnitude, right ascension, right ascension rate, magnitude of the velocity vector and velocity azimuth; C3 energy, incoming and outgoing asymptotes and other target vectors; Vector components, dot products and angles between vectors; User variable values
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ASTROGATOR |