SE442851B - Forfarande och anordning vid styrsystem - Google Patents
Forfarande och anordning vid styrsystemInfo
- Publication number
- SE442851B SE442851B SE8302136A SE8302136A SE442851B SE 442851 B SE442851 B SE 442851B SE 8302136 A SE8302136 A SE 8302136A SE 8302136 A SE8302136 A SE 8302136A SE 442851 B SE442851 B SE 442851B
- Authority
- SE
- Sweden
- Prior art keywords
- characteristic
- control
- equipment
- actuator
- exhibition
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims description 9
- 230000003247 decreasing effect Effects 0.000 claims abstract 8
- 230000007935 neutral effect Effects 0.000 claims description 13
- 238000004364 calculation method Methods 0.000 claims description 7
- 230000001419 dependent effect Effects 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims 1
- 238000006073 displacement reaction Methods 0.000 abstract 6
- 238000010586 diagram Methods 0.000 description 10
- 238000004422 calculation algorithm Methods 0.000 description 9
- 238000012937 correction Methods 0.000 description 5
- 230000002787 reinforcement Effects 0.000 description 5
- 230000007423 decrease Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000010355 oscillation Effects 0.000 description 2
- 101100298295 Drosophila melanogaster flfl gene Proteins 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 238000004590 computer program Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 230000036962 time dependent Effects 0.000 description 1
- 238000009966 trimming Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Control Of Position Or Direction (AREA)
- Feedback Control In General (AREA)
- Threshing Machine Elements (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
- Control Of Eletrric Generators (AREA)
- Mechanical Control Devices (AREA)
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE8302136A SE442851B (sv) | 1983-04-18 | 1983-04-18 | Forfarande och anordning vid styrsystem |
| AT84850127T ATE41536T1 (de) | 1983-04-18 | 1984-04-17 | Verfahren um in einem steuersystem die antwortgenauigkeit zu veraendern. |
| DE8484850127T DE3477277D1 (en) | 1983-04-18 | 1984-04-17 | Method of varying response fineness in a control system |
| EP84850127A EP0123665B1 (de) | 1983-04-18 | 1984-04-17 | Verfahren um in einem Steuersystem die Antwortgenauigkeit zu verändern |
| US06/601,644 US4589061A (en) | 1983-04-18 | 1984-04-18 | Method of varying response fineness in a control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE8302136A SE442851B (sv) | 1983-04-18 | 1983-04-18 | Forfarande och anordning vid styrsystem |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| SE8302136D0 SE8302136D0 (sv) | 1983-04-18 |
| SE8302136L SE8302136L (sv) | 1984-10-19 |
| SE442851B true SE442851B (sv) | 1986-02-03 |
Family
ID=20350831
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SE8302136A SE442851B (sv) | 1983-04-18 | 1983-04-18 | Forfarande och anordning vid styrsystem |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4589061A (de) |
| EP (1) | EP0123665B1 (de) |
| AT (1) | ATE41536T1 (de) |
| DE (1) | DE3477277D1 (de) |
| SE (1) | SE442851B (de) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU569780B2 (en) * | 1984-03-15 | 1988-02-18 | Alfred Leslie Gilmore | Improvements to bore hole pump sets |
| JPS61128319A (ja) * | 1984-11-28 | 1986-06-16 | Nippon Kogaku Kk <Nikon> | 駆動装置 |
| JPS6368913A (ja) * | 1986-09-10 | 1988-03-28 | Fujitsu Ltd | サ−ボ制御回路 |
| US5489830A (en) * | 1994-09-09 | 1996-02-06 | Mcdonnell Douglas Corporation | Control system with loadfeel and backdrive |
| US6559833B2 (en) | 1998-10-01 | 2003-05-06 | Hewlett-Packard Development Company | Apparatus and method for achieving absolute and relative positioning of a graphics cursor |
| JP3925527B2 (ja) | 2004-10-01 | 2007-06-06 | セイコーエプソン株式会社 | 液滴吐出装置、パネルの製造方法、画像表示装置および電子機器 |
| FR3030449B1 (fr) * | 2014-12-19 | 2017-11-24 | Airbus Operations Sas | Procede et systeme de commande de direction pour un aeronef |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1154853B (de) * | 1961-06-27 | 1963-09-26 | Continental Elektro Ind Ag | Einrichtung zur elektrischen Steuerung eines einem bewegten Objekt nachzufuehrenden Richtmittels |
| DE1224398B (de) * | 1962-08-18 | 1966-09-08 | Siemens Ag | Anordnungen zur Begrenzung des Stellbereiches eines Stellantriebs |
| US3644720A (en) * | 1969-10-06 | 1972-02-22 | Chandler Evans Inc | Gain multiplier |
| US4052598A (en) * | 1976-05-03 | 1977-10-04 | Hycom Incorporated | Control system with fast response |
| DE2807902C2 (de) * | 1978-02-24 | 1980-04-30 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Steuereinrichtung mit aktiver Kraft rückführung |
| US4218733A (en) * | 1978-11-13 | 1980-08-19 | Sybron Corporation | Adaptive gain controller |
-
1983
- 1983-04-18 SE SE8302136A patent/SE442851B/sv not_active IP Right Cessation
-
1984
- 1984-04-17 AT AT84850127T patent/ATE41536T1/de not_active IP Right Cessation
- 1984-04-17 DE DE8484850127T patent/DE3477277D1/de not_active Expired
- 1984-04-17 EP EP84850127A patent/EP0123665B1/de not_active Expired
- 1984-04-18 US US06/601,644 patent/US4589061A/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP0123665A3 (en) | 1986-01-08 |
| DE3477277D1 (en) | 1989-04-20 |
| ATE41536T1 (de) | 1989-04-15 |
| US4589061A (en) | 1986-05-13 |
| SE8302136L (sv) | 1984-10-19 |
| EP0123665A2 (de) | 1984-10-31 |
| SE8302136D0 (sv) | 1983-04-18 |
| EP0123665B1 (de) | 1989-03-15 |
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Legal Events
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| NAL | Patent in force |
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