Technology report - guidance and control engineering.
Guidance and control technology examining inertial guidance systems, Apollo space system, gyros, accelerometers and computers
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Guidance and control technology examining inertial guidance systems, Apollo space system, gyros, accelerometers and computers
Small, lightweight angular accelerometer performs reliably when subjected to harsh temperature and vibration environments. The device uses strain gages to measure the amount of deflection in a metal ring caused by movement of inertial masses mounted through the ring. Range of the instrument is varied by varying the value of inertial masses.
Effect of transducer impedance on dynamic measurements - frequency limit for accelerometer
Servoamplifier and amplifier-detector inspection for gyroscope and accelerometer servo loops
Inertial measurement unit, pulsed integrating pendulous accelerometer, and coupling data unit of Apollo guidance and control system
Angular accelerometers and transducers compared in detection of seismic waves and shear waves
Coordinated orbital technology experiment program discussing guidance and control, ground test, low-g accelerometer test, error sources, elimination, etc
Ferromagnetic fluid developing body force under magnetic field influence, noting changes in internal pressure, velocity, etc, applied to attitude control devices, accelerometers, etc
Static testing program on cryogenic fuel density measurement, mass flow meters, damped accelerometers, and digital transducer
Design feasibility of precision tilt and angular vibration isolation system using gyroscope and accelerometer instruments for control
Accelerometer for airborne measurements of vestibular forces acting on helicopter pilots
Impact acceleration measured by accelerometers and FM/AM telemetry
Scanning techniques for random noise and vibration testing of spacecraft using multiple channel accelerometer
Pendulum device producing low level quasi-static accelerations for accelerometer calibration
Analog-to-digital computer accepts physiological flight data as three basic analog input signals - the ECG signal, the flowmeter signal which is a respiration monitor, and the accelerometer signal which measures the normal-g-load on the subject.
Mathematical models for testing strapdown system with pendulous integrating gyro accelerometer
Thermal performance of pressure transducers, accelerometers, displacement transducers, resistance thermometers and control mechanisms for NERVA reactor
FM/AM telemetry circuits with three axis piezoelectric accelerometer for measurements during impact tests of soft landing models