Skip to main content

  • Result of

  • « Previous
    Next »

Correction for atmospheric refraction at the NASA minitrack stations / F.O. Vonbun

Thumbnail for Correction for atmospheric refraction at the NASA minitrack stations / F.O. Vonbun
View
@ University of Illinois

Vonbun, F.O

Description

Cover title."August 1962."Communications and tracking installations, ground; Navigation and navigation equipment; Physics, theoretical; Simulators and computers.Includes bibliographical references.
Type:
Text
Format:
Language Material Electronic Resource
Contributors:
United States. National Aeronautics and Space Administration
Rights:
Public domain. Learn more at http://www.hathitrust.org/access_use
View Original At:

Record Contributed By

University of Illinois

Record Harvested From

HathiTrust

Keywords

  1. Communications And Tracking Installations, Ground
  2. Navigation And Navigation Equipment
  3. Physics, Theoretical
  4. Simulators And Computers

Related Content

An investigation of the effects of the time lag due to long transmission distance upon remote control: Phase II - Vehicle experiments, Phase III - Conclusions Computational procedure for Vinti's theory of an accurate intermediary orbit Piloted simulator tests of a guidance system which can continuously predict landing point of a low L/D vehicle during atmosphere re-entry Pulse frequency modulation Fourier series operating package A digital command system for satellites NASA Scout ST-1 flight-test results and analyses, launch operations and test vehicle description Effects of gyroscopic cross coupling between pitch and roll on the handling qualities of VTOL aircraft Air-helium simulation of the aerodynamic force coefficients of cones at hypersonic speeds VTOL height-control requirements in hovering as determined from motion simulation study Simulator studies of simple attitude control for spin-stabilized vehicles Analog-computer investigation of effects of friction and preload on the dynamic longitudinal characteristics of a pilot-airplane combination. Monte Carlo calculations of neutron number sprectra and buildup factors in infinite conical configurations / Millard L. Wohl Spacecraft information systems Attitude control requirements for hovering determined through the use of a piloted flight simulator Review of the X-15 program Joseph Weil Human pilots' dynamic response characteristics measured in flight and on a nonmoving simulator A preliminary piloted simulator and flight study of height control requirements for VTOL aircraft Efflux of thermal radiation from a cylindrical cavity irradiated from an external source A flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle
Download JSON