Questions tagged [rotation-sequences]
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Rotation matrix / coordinate transformation of maneuver parameters from Prograde, Normal, Radial to Cartesian XYZ?
Say I have a state vector and Keplerian elements of an orbiting spacecraft:
Position = [x, y, z]
Velocity = [vx, vy, vz]
Elements = [a, e, i, $\omega$, $\Omega$, $\nu$]
And I have the maneuver I ...
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1answer
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Converting J2000 to ECEF?
Say I get the orbital elements for the ISS from JPL Horizons.
Say that data is expressed in J2000, an inertial frame. I want to express it in ECEF.
This is a simple rotation transform. All I need is ...
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Why no yaw in ADI when LVLH is selected?
The space shuttle would display the spacecraft's attitude in one of three frames: LVLH, REF, or INRTL.
Launch procedures called for LVLH to be selected very early in launch.
The attitude indicator ...