GB854906A - Flight aid systems for rotary wing aircraft - Google Patents
Flight aid systems for rotary wing aircraftInfo
- Publication number
- GB854906A GB854906A GB19739/60A GB1973960A GB854906A GB 854906 A GB854906 A GB 854906A GB 19739/60 A GB19739/60 A GB 19739/60A GB 1973960 A GB1973960 A GB 1973960A GB 854906 A GB854906 A GB 854906A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aid systems
- wing aircraft
- rotary wing
- flight aid
- jan
- 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
- 230000001133 acceleration Effects 0.000 abstract 1
- 238000006073 displacement reaction Methods 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
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
-
- 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)
- Traffic Control Systems (AREA)
- Toys (AREA)
Abstract
854,906. Aircraft flight aid systems. SPERRY RAND CORPORATION. Jan. 1, 1957 [Jan. 3, 1956], No. 19739/60. Divided out of 854,904. Drawings to Specification. Class 40 (1). The description is the same as that of Specification 854,904, but the claims are for a system comprising means for deriving an error signal representing the difference between actual and desired craft altitude, and means for algebraically combining this error signal with a further signal representing either vertical acceleration or the displacement of the collective pitch control means. The system is particularly suitable for enabling the pilot of a helicopter to approach and maintain a desired altitude. Specifications 854,905 and 854,907 also are referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US854906XA | 1956-01-03 | 1956-01-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB854906A true GB854906A (en) | 1960-11-23 |
Family
ID=22191947
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB19739/60A Expired GB854906A (en) | 1956-01-03 | 1957-01-01 | Flight aid systems for rotary wing aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB854906A (en) |
-
1957
- 1957-01-01 GB GB19739/60A patent/GB854906A/en not_active Expired
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