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ATTITUDE DYNAMICS AND CONTROL
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acceleration aluminum angle angular momentum antenna apogee apogee motor approximately Ariane assumed attitude control axes axial band bandwidth battery beam communications satellites components configuration constant determined discharge dissipation dual-spin-stabilized spacecraft dynamic earth station eclipse electric power electrons elements energy equation equinox equipment error factor Figure function geosynchronous orbit given heat pipe hydrazine inclination inertia Intelsat ion thrusters launch vehicle load longitude maneuvers matrix maximum microwave modulation momentum wheel motion natural frequency node normal nutation output panel payload perigee perturbing plane propellant propulsion radiation ratio reflector regulator right ascension rotating sensor shown in Fig shunt Shuttle signal sinusoidal solar array solar cell space spacecraft spacecraft structure specific impulse spectrum spin axis stabilization station keeping stress summer solstice surface synchronous orbit techniques temperature thermal control three-axis-stabilized spacecraft thrusters torque transfer orbit TWTAs typical vector zero