GB854734A - Aircraft guidance apparatus - Google Patents
Aircraft guidance apparatusInfo
- Publication number
- GB854734A GB854734A GB35090/58A GB3509058A GB854734A GB 854734 A GB854734 A GB 854734A GB 35090/58 A GB35090/58 A GB 35090/58A GB 3509058 A GB3509058 A GB 3509058A GB 854734 A GB854734 A GB 854734A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- flight path
- signal dependent
- guidance apparatus
- displacement
- 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
Links
- 230000001419 dependent effect Effects 0.000 abstract 3
- 238000006073 displacement reaction Methods 0.000 abstract 2
- 230000010354 integration Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
854,734. Automatic steering control systems. SPERRY RAND CORPORATION. Feb. 15, 1957 [March 15, 1956], No. 35090/58. Divided out of 854,732. Drawings to Specification. Class 38 (4). The subject-matter of this Specification is identical with that of Specification 854,732 but the claims relate to aircraft guidance apparatus in which a signal dependent on displacement of the aircraft from a predetermined flight path, a signal dependent on rate of change of displacement of the aircraft from the flight path obtained by integration of the output of a linear accelerometer, and a signal dependent on deviation of attitude from that which is normal when on the flight path, are combined in a particular algebraic manner. Specifications 854,733 and 854,735 also are referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US854734XA | 1956-03-15 | 1956-03-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB854734A true GB854734A (en) | 1960-11-23 |
Family
ID=22191842
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB35090/58A Expired GB854734A (en) | 1956-03-15 | 1957-02-15 | Aircraft guidance apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB854734A (en) |
-
1957
- 1957-02-15 GB GB35090/58A patent/GB854734A/en not_active Expired
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