GB814744A - Improvements in world wide navigational system - Google Patents

Improvements in world wide navigational system

Info

Publication number
GB814744A
GB814744A GB3734655A GB3734655A GB814744A GB 814744 A GB814744 A GB 814744A GB 3734655 A GB3734655 A GB 3734655A GB 3734655 A GB3734655 A GB 3734655A GB 814744 A GB814744 A GB 814744A
Authority
GB
United Kingdom
Prior art keywords
craft
earth
angle
gyroscope
reference unit
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB3734655A
Inventor
John Wightman Gray
Everett Burton Hales
Evan Anderson Greenwood Jr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Precision Laboratory Inc
Original Assignee
General Precision Laboratory Inc
Filing date
Publication date
Application filed by General Precision Laboratory Inc filed Critical General Precision Laboratory Inc
Publication of GB814744A publication Critical patent/GB814744A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/50Systems of measurement based on relative movement of target
    • G01S13/58Velocity or trajectory determination systems; Sense-of-movement determination systems
    • G01S13/60Velocity or trajectory determination systems; Sense-of-movement determination systems wherein the transmitter and receiver are mounted on the moving object, e.g. for determining ground speed, drift angle, ground track

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)

Abstract

814,744. Radio-direction finding. GENERAL PRECISION LABORATORY Inc. Dec. 29, 1955, No. 37346/55. Drawings to Specification. Class 40 (7). [Also in Group XX] In an aircraft great circle, radio-echo navigation system in which a craft may home on a selected point without terrestial or celestial fixes, other than the initial one, to allow for the inaccuracies introduced by the convergence of meridians at the Poles of the Earth, the computing co-ordinate system is automatically rotated by one right-angle to form a transverse co-ordinate system, when the craft is at a specified distance from the Poles. The integrators which compute the instantaneous craft position operate in terms of the transverse co-ordinate system and can owing to the coordinate change, operate normally so as to continuously integrate the orthogonal components of the ground speed vector. The craft ground speed and drift angle are determined by a Doppler radar system of the pulse type, having three directive arrays to provide forward and laterally directed beams inclined towards the Earth. The ground track angle is determined by a heading reference unit which combines the heading angle with the drift angle. The instantaneous latitude and longitude, which are computed by combining the outputs of the Doppler system and the reference unit, are applied to a second computer which derives the great circle course and the distance to destination. The output of the magnetic compass of the heading reference unit is stabilized against high-frequency oscillations by a feed-back loop and when, at the North Pole, it fails to function, it is replaced by a directional gyroscope. In addition, a correction for magnetic variation with position is added. The gyroscope is normally monitored from the magnetic compass by means of a second feed-back loop which is supplied with information from the longitude and latitude computer which corrects the gyroscope for both the Earth's rotation and the relative movement of the craft and Earth.
GB3734655A 1955-12-29 Improvements in world wide navigational system Expired GB814744A (en)

Publications (1)

Publication Number Publication Date
GB814744A true GB814744A (en) 1959-06-10

Family

ID=34317897

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3734655A Expired GB814744A (en) 1955-12-29 Improvements in world wide navigational system

Country Status (1)

Country Link
GB (1) GB814744A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9562788B1 (en) * 2011-09-30 2017-02-07 Rockwell Collins, Inc. System and method for doppler aided navigation using weather radar
US9733349B1 (en) 2007-09-06 2017-08-15 Rockwell Collins, Inc. System for and method of radar data processing for low visibility landing applications
US9939526B2 (en) 2007-09-06 2018-04-10 Rockwell Collins, Inc. Display system and method using weather radar sensing
US10228460B1 (en) 2016-05-26 2019-03-12 Rockwell Collins, Inc. Weather radar enabled low visibility operation system and method
US10353068B1 (en) 2016-07-28 2019-07-16 Rockwell Collins, Inc. Weather radar enabled offshore operation system and method
US10705201B1 (en) 2015-08-31 2020-07-07 Rockwell Collins, Inc. Radar beam sharpening system and method
US10928510B1 (en) 2014-09-10 2021-02-23 Rockwell Collins, Inc. System for and method of image processing for low visibility landing applications
CN114001731A (en) * 2021-10-12 2022-02-01 苏州大学 Polar region inertial navigation phase modulation damping method and system under virtual sphere model

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9733349B1 (en) 2007-09-06 2017-08-15 Rockwell Collins, Inc. System for and method of radar data processing for low visibility landing applications
US9939526B2 (en) 2007-09-06 2018-04-10 Rockwell Collins, Inc. Display system and method using weather radar sensing
US9562788B1 (en) * 2011-09-30 2017-02-07 Rockwell Collins, Inc. System and method for doppler aided navigation using weather radar
US10928510B1 (en) 2014-09-10 2021-02-23 Rockwell Collins, Inc. System for and method of image processing for low visibility landing applications
US10705201B1 (en) 2015-08-31 2020-07-07 Rockwell Collins, Inc. Radar beam sharpening system and method
US10228460B1 (en) 2016-05-26 2019-03-12 Rockwell Collins, Inc. Weather radar enabled low visibility operation system and method
US10955548B1 (en) 2016-05-26 2021-03-23 Rockwell Collins, Inc. Weather radar enabled low visibility operation system and method
US10353068B1 (en) 2016-07-28 2019-07-16 Rockwell Collins, Inc. Weather radar enabled offshore operation system and method
CN114001731A (en) * 2021-10-12 2022-02-01 苏州大学 Polar region inertial navigation phase modulation damping method and system under virtual sphere model
CN114001731B (en) * 2021-10-12 2023-03-07 苏州大学 Polar region inertial navigation phase modulation damping method and system under virtual sphere model

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