GB835265A - Aircraft navigation apparatus - Google Patents

Aircraft navigation apparatus

Info

Publication number
GB835265A
GB835265A GB32709/59A GB3270959A GB835265A GB 835265 A GB835265 A GB 835265A GB 32709/59 A GB32709/59 A GB 32709/59A GB 3270959 A GB3270959 A GB 3270959A GB 835265 A GB835265 A GB 835265A
Authority
GB
United Kingdom
Prior art keywords
navigation apparatus
course
aircraft navigation
aircraft
manuallyadjustable
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
GB32709/59A
Inventor
Frank Dove
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.)
Sperry Gyroscope Co Ltd
Original Assignee
Sperry Gyroscope Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Sperry Gyroscope Co Ltd filed Critical Sperry Gyroscope Co Ltd
Priority to GB32709/59A priority Critical patent/GB835265A/en
Publication of GB835265A publication Critical patent/GB835265A/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/0202—Control of position or course in two dimensions specially adapted to aircraft

Abstract

835,265. Automatic steering control systems. SPERRY GYROSCOPE CO. Ltd. June 22, 1956, No. 32709/59. Divided out of 835,264. Drawings to Specification. Class 38 (4). The subject-matter of this Specification is identical with that of Specification 835,264 but the claims are directed to a system for automatically piloting an aircraft in azimuth in which the course to be steered is set by manually adjusting a member associated with an indicator to one of a plurality of positions, and servo means may be brought into operation subsequently, whenever desired, to move course adjusting means for the automatic pilot to a position corresponding to that of the manuallyadjustable member.
GB32709/59A 1956-06-22 1956-06-22 Aircraft navigation apparatus Expired GB835265A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB32709/59A GB835265A (en) 1956-06-22 1956-06-22 Aircraft navigation apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB32709/59A GB835265A (en) 1956-06-22 1956-06-22 Aircraft navigation apparatus

Publications (1)

Publication Number Publication Date
GB835265A true GB835265A (en) 1960-05-18

Family

ID=10342839

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32709/59A Expired GB835265A (en) 1956-06-22 1956-06-22 Aircraft navigation apparatus

Country Status (1)

Country Link
GB (1) GB835265A (en)

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