PRECISION VELOCITY MEASUREMENT FOR INERTIAL GUIDANCE TESTING

Abstract

Two practical solutions are advanced to the problem of measuring the velocity of the center of gravity of a rocket sled to 1 part in 10 to the 5th power over a speed range of 200 to 5,000 ft/sec. Solutions are based on a combined space-time/accelerometer system. The characteristics of the systems and the manner in which they meet the requirements are discussed and a program is outlined whereby either system may be introduced as the standard velocity measuring system for the sled test facility at the Air Force Missile Development Center. In reaching the conclusion that the combined space-time/accelerometer system is the optimum solution, other methods were investigated. Results of these studies of direct physical methods, as well as methods from which velocity may be inferred, are discussed. None of the methods examined was found to offer a satisfactory solution to the problem at hand. I is poi d out that quality of instrumentation must be paramount in developing any velocity measuring system and no amount of statistical operations with the data can compensate for data of poor quality. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1961
Accession Number
AD0266737

Entities

People

  • Peter Felsenthal
  • Thomas B. Smith
  • William D. Jr. Green

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accelerometers
  • Air Force
  • Center Of Gravity
  • Guidance
  • Inertial Navigation
  • Instrumentation
  • Measurement
  • Measuring Instruments
  • Rocket Sleds
  • Sled Tests
  • Sleds
  • Test Facilities

Readers

  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Space Exploration and Orbital Mechanics.
  • Systems Analysis and Design

Technology Areas

  • AI & ML
  • AI & ML - Bayesian Inference
  • AI & ML - DoD AI Strategy
  • Space
  • Space - Hall-Effect Thruster