FR1203524A - Auto-correcting aircraft navigation system - Google Patents

Auto-correcting aircraft navigation system

Info

Publication number
FR1203524A
FR1203524A FR1203524DA FR1203524A FR 1203524 A FR1203524 A FR 1203524A FR 1203524D A FR1203524D A FR 1203524DA FR 1203524 A FR1203524 A FR 1203524A
Authority
FR
France
Prior art keywords
auto
navigation system
aircraft navigation
correcting
correcting aircraft
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
Other languages
French (fr)
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.)
Lear Inc
Original Assignee
Lear Inc
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 Lear Inc filed Critical Lear Inc
Application granted granted Critical
Publication of FR1203524A publication Critical patent/FR1203524A/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
    • G01C21/188—Compensation of inertial measurements, e.g. for temperature effects for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
FR1203524D 1958-02-06 1958-02-06 Auto-correcting aircraft navigation system Expired FR1203524A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1203524T 1958-02-06

Publications (1)

Publication Number Publication Date
FR1203524A true FR1203524A (en) 1960-01-19

Family

ID=9672479

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1203524D Expired FR1203524A (en) 1958-02-06 1958-02-06 Auto-correcting aircraft navigation system

Country Status (1)

Country Link
FR (1) FR1203524A (en)

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