DE1431190B2 - - Google Patents
Info
- Publication number
- DE1431190B2 DE1431190B2 DE19641431190 DE1431190A DE1431190B2 DE 1431190 B2 DE1431190 B2 DE 1431190B2 DE 19641431190 DE19641431190 DE 19641431190 DE 1431190 A DE1431190 A DE 1431190A DE 1431190 B2 DE1431190 B2 DE 1431190B2
- Authority
- DE
- Germany
- Prior art keywords
- voltage
- capacitor
- circuit
- threshold value
- signal
- 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.)
- Pending
Links
- 239000003990 capacitor Substances 0.000 claims description 24
- 230000006641 stabilisation Effects 0.000 claims description 14
- 238000011105 stabilization Methods 0.000 claims description 14
- 238000004804 winding Methods 0.000 description 26
- 230000000694 effects Effects 0.000 description 4
- 230000000087 stabilizing effect Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
-
- 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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
-
- 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
-
- 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
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)
- Mechanical Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Amplifiers (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US284707A US3199013A (en) | 1963-05-31 | 1963-05-31 | Rate responsive compensation change circuit |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE1431190A1 DE1431190A1 (de) | 1969-01-16 |
| DE1431190B2 true DE1431190B2 (US07608600-20091027-C00054.png) | 1970-10-29 |
Family
ID=23091221
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19641431190 Pending DE1431190A1 (de) | 1963-05-31 | 1964-05-29 | Stabilisierungssystem fuer Flugzeuge |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3199013A (US07608600-20091027-C00054.png) |
| DE (1) | DE1431190A1 (US07608600-20091027-C00054.png) |
| FR (1) | FR1426125A (US07608600-20091027-C00054.png) |
| GB (1) | GB1070211A (US07608600-20091027-C00054.png) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3949696A (en) * | 1972-06-21 | 1976-04-13 | Tokyo Keiki Company Limited | Marine steering arrangement |
| US3908935A (en) * | 1974-04-19 | 1975-09-30 | Pneumo Dynamics Corp | Aircraft duplex system |
| US4460858A (en) * | 1982-05-11 | 1984-07-17 | The Boeing Company | Autopilot roll control wheel steering system |
| US4536689A (en) * | 1984-05-17 | 1985-08-20 | Sperry Corporation | Servomotor feedback fault detector |
| US5079492A (en) * | 1988-03-29 | 1992-01-07 | Teijin Seiki Company Limited | Stability compensating circuit |
| JPH01248211A (ja) * | 1988-03-29 | 1989-10-03 | Teijin Seiki Co Ltd | 安定性補償回路 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2762962A (en) * | 1950-06-21 | 1956-09-11 | Smith & Sons Ltd S | Safety device for automatic pilot system |
| US2973650A (en) * | 1954-11-16 | 1961-03-07 | Sperry Gyroscope Co Ltd | Safety device for control systems for aircraft |
-
1963
- 1963-05-31 US US284707A patent/US3199013A/en not_active Expired - Lifetime
-
1964
- 1964-05-19 GB GB20656/64A patent/GB1070211A/en not_active Expired
- 1964-05-29 DE DE19641431190 patent/DE1431190A1/de active Pending
- 1964-06-01 FR FR4695A patent/FR1426125A/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR1426125A (fr) | 1966-01-28 |
| DE1431190A1 (de) | 1969-01-16 |
| US3199013A (en) | 1965-08-03 |
| GB1070211A (en) | 1967-06-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| E77 | Valid patent as to the heymanns-index 1977 |