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Accelerometers
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A Study of the Critical Computational Problems Associated with Strapdown Inertial Navigation Systems
Recent Developments in Wind Tunnel Measurements of Aerodynamic Derivatives
Sinusoidal Vibration Tests on Development Model of Experiment S-126 for Td-2 Spacecraft
Low Altitude Turbulence Measurements over Land and Sea During Flights in a Canberra Aircraft
Use of an Aircraft for Measuring the Statistical Distribution of Turbulence
Description and Performance of the Saturn Launch Vehicle's Navigation, Guidance, and Control System
Developments in Navigation and Measurement of Gravity at Sea
Detection of Titan Pogo Characteristics by Analysis of Random Data
Advanced Research in Guidance, Control, and Instrumentation
Vibration Levels Experienced in Take-off on a Large Flexible Aircraft
Measurement of the Yawing Moment of Inertia of an Aircraft (Hp115) IN Flight
Development of an Improved Sensitive Triaxial Piezoelectric Accelerometer
Integrated Navigation Satellite/Inertial System Flight Test Analysis
Piezoelectric Triaxial Accelerometer System for Use in Satellite Air Density Measurements
Piezoelectric Triaxial Accelerometer System for Use in Satellite Air Density Measurements
Development and Evaluation of Automobile Crash Sensors--Executive Summary
High Altitude Supersonic Target (HAST) KJ-4 Guidance and Control System Analysis
Development, Test, and Calibration of a Three-Axis Accelerometer System
Micro-g Triaxial Piezoelectric Satellite Accelerometer System Development
Flutter Prediction for a Wing with Active Aileron Control
Flight and Analytical Investigations of a Structural Mode Excitation System on the YF-12A Airplane
Superconducting Gravity Gradiometer Mission. Volume 2. Study Team Technical Report
Superconducting Gravity Gradiometer Mission. Volume 1: Study Team Executive Summary
Gyrometre Laser Triaxial Miniaturise (Miniaturized Triaxial Laser Gyro)
Comparison of Low-Gravity Measurements on-Board Columbia during STS-40
USML-1 Microgravity Glovebox Experiment No. 1 Passive Accelerometer System
Application of Roll-Isolated Inertial Measurement Units to the Instrumentation of Spinning Vehicles