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The Editor Reports
A New Guiding and Tracking System Henry P Kalmus
Criterion for Angular Noise in StarLock Systems E K Sandeman
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accelerometer aerospace Air Traffic Control aircraft amplitude amplitude modulation angular antenna application autocorrelation automatic Aviation axis bandwidth beam carrier frequency channel characteristics circuit communication system components constant correlation curve demodulation detector deviation digital communication display distance distribution Doppler Doppler radar drift-rate Electronics equations equipment error filter flight function gimbal gyro drift rate indicated inertial inertial guidance system input integral leakage rejection limited lock telescope mask mean-square ment method miles misalignment mode Model multipath navigation noise term obtained on-time operation output parameters path PGANE phase modulation photofrequency photon noise position propagation pulse quency radar system radio random range ratio receiver secondary surveillance radar selected shown in Fig signal Sinusoidal Spirals space spiral star image star-image track star-lock system station storage switch techniques tion torque tracker trans transfer function transmission transmitted transponder vector velocity voltage zero