ASD Technical Report, Numéros 63 à 74

0-DEGREE INCLINATION 120 degrees Right 15 degrees 240 degrees Pitch 4-79 Mopermalloy 90 degrees actuation system Air Arm Division Altitude amplifiers attitude control attitude errors Bendix Corporation Calif coil currents coil torque CONTROLLER WEIGHT cores are superior curve DATA degrees Pitch Roll degrees Right Ascension Dept direct actuation Disturbance Level disturbance torques Division ATTN dyne-cm DYNE-CM/GAUSS earth's field earth's magnetic field electromagnetic Engineering ATTN ferromagnetic ferromagnetic cores flux density function gauss Geomagnetic Field Components indirect system K₁ magnetic actuators magnetic field components magnetic torquers magnetometer meter miles milligauss NON-GOVERNMENT ORGANIZATIONS North American Aviation Optimum Weight Orbit Position P. O. Box PEAK ERROR Peak Position Error permanent magnet Pitch Roll Yaw Position Degrees reaction wheels residual torque Roll Yaw Pitch shown in figure SIMULATION RESULTS TABLE three orthogonal coils UNCLASSIFIED REPORT values variety of orbits vector vehicle momentum Westinghouse Electric Corporation WHEEL MOMENTUM Yaw Component Yaw Pitch Roll