IL102482A - Seyal introduction limit to control system - Google Patents
Seyal introduction limit to control systemInfo
- Publication number
- IL102482A IL102482A IL10248292A IL10248292A IL102482A IL 102482 A IL102482 A IL 102482A IL 10248292 A IL10248292 A IL 10248292A IL 10248292 A IL10248292 A IL 10248292A IL 102482 A IL102482 A IL 102482A
- Authority
- IL
- Israel
- Prior art keywords
- prime mover
- rate
- control system
- signal
- line
- Prior art date
Links
- 230000003044 adaptive effect Effects 0.000 title claims description 5
- 230000008859 change Effects 0.000 claims description 13
- 230000004044 response Effects 0.000 claims description 7
- 238000013459 approach Methods 0.000 claims description 3
- 230000007423 decrease Effects 0.000 description 7
- 238000012360 testing method Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 238000012544 monitoring process Methods 0.000 description 4
- 230000001133 acceleration Effects 0.000 description 3
- 125000004122 cyclic group Chemical group 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 238000007792 addition Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 230000009528 severe injury Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B5/00—Anti-hunting arrangements
- G05B5/01—Anti-hunting arrangements electric
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S424/00—Drug, bio-affecting and body treating compositions
- Y10S424/819—Viral vaccine for feline species, e.g. cats
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Feedback Control In General (AREA)
- Control Of Position Or Direction (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/733,793 US5224664A (en) | 1991-07-22 | 1991-07-22 | Adaptive control system input limiting |
Publications (2)
Publication Number | Publication Date |
---|---|
IL102482A0 IL102482A0 (en) | 1993-02-21 |
IL102482A true IL102482A (en) | 1996-05-14 |
Family
ID=24949140
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL10248292A IL102482A (en) | 1991-07-22 | 1992-07-13 | Seyal introduction limit to control system |
Country Status (10)
Country | Link |
---|---|
US (1) | US5224664A (de) |
EP (1) | EP0595914B1 (de) |
JP (1) | JPH06509198A (de) |
KR (1) | KR100233345B1 (de) |
AU (1) | AU657157B2 (de) |
CA (1) | CA2113648C (de) |
DE (1) | DE69206805T2 (de) |
ES (1) | ES2083752T3 (de) |
IL (1) | IL102482A (de) |
WO (1) | WO1993002405A1 (de) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2114022C (en) * | 1991-08-28 | 2000-09-19 | Phillip J. Gold | Vertical control system for rotary wing aircraft |
US5377937A (en) * | 1991-09-03 | 1995-01-03 | The Boeing Company | Aircraft flare control system utilizing an envelope limiter |
US5264768A (en) * | 1992-10-06 | 1993-11-23 | Honeywell, Inc. | Active hand controller feedback loop |
FR2711257B1 (fr) * | 1993-10-14 | 1995-12-22 | Aerospatiale | Système de commande de vol électrique pour avion avec protection en assiette au décollage. |
DE4421105A1 (de) * | 1993-11-02 | 1995-05-04 | Hewlett Packard Co | Reduzierung des elektrischen Motorstoßstroms durch nicht-lineare Begrenzung der Änderungsrate der Winkelgeschwindigkeit |
US5826834A (en) * | 1994-10-19 | 1998-10-27 | Honeywell Inc. | Self adaptive limiter for automatic control of approach and landing |
US5850615A (en) * | 1995-12-06 | 1998-12-15 | Mcdonnell Douglas Helicopter Co. | Rotor blade swashplate-axis rotation and gyroscopic moments componsator |
WO1997020734A2 (en) * | 1995-12-06 | 1997-06-12 | Mc Donnell Douglas Corporation | Flight control system for jet powered tri-mode aircraft |
FR2756252B1 (fr) * | 1996-11-22 | 1999-01-22 | Eurocopter France | Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere |
US6003811A (en) * | 1997-03-24 | 1999-12-21 | The Boeing Company | Aircraft servovalve current rate limiter |
US6021370A (en) * | 1997-08-05 | 2000-02-01 | Cummins Engine Company, Inc. | Vehicle/engine acceleration rate management system |
SE508672C2 (sv) * | 1997-12-30 | 1998-10-26 | Saab Ab | Anordning och metod för styrkraftreglering vid ett mekaniskt styrsystem för ett flygplan |
JP3195918B2 (ja) * | 1999-03-12 | 2001-08-06 | 株式会社コミュータヘリコプタ先進技術研究所 | ヘリコプタ用飛行制御装置 |
US6422517B1 (en) | 1999-12-02 | 2002-07-23 | Boeing Company | Aircraft tailstrike avoidance system |
US6618631B1 (en) | 2000-04-25 | 2003-09-09 | Georgia Tech Research Corporation | Adaptive control system having hedge unit and related apparatus and methods |
US6885917B2 (en) | 2002-11-07 | 2005-04-26 | The Boeing Company | Enhanced flight control systems and methods for a jet powered tri-mode aircraft |
GB2412976B (en) | 2002-12-09 | 2006-07-26 | Georgia Tech Res Inst | Adaptive output feedback apparatuses and methods capable of controlling a nonminimum phase system |
DE10323785B4 (de) * | 2003-05-23 | 2009-09-10 | Wobben, Aloys, Dipl.-Ing. | Verfahren zum Erkennen eines Eisansatzes an Rotorblättern |
US7463956B2 (en) * | 2003-07-03 | 2008-12-09 | The Boeing Company | Constant vertical state maintaining cueing system |
US7627403B2 (en) * | 2006-03-23 | 2009-12-01 | The Boeing Company | Bias correcting phase compensating rate limiter |
US7617024B2 (en) * | 2006-09-22 | 2009-11-10 | Bell Helicopter Textron Inc. | Automatic heading control system for tiltrotor aircraft and helicopters |
FR2920231B1 (fr) * | 2007-08-20 | 2015-02-27 | Airbus France | Procede et dispositif de protection automatique d'un aeronef contre un atterissage dur |
US8002220B2 (en) * | 2007-10-25 | 2011-08-23 | Honeywell International Inc. | Rate limited active pilot inceptor system and method |
US7988089B2 (en) * | 2008-03-27 | 2011-08-02 | Sikorsky Aircraft Corporation | Swashplate trajectory control |
JP5893890B2 (ja) * | 2011-10-18 | 2016-03-23 | 三菱重工業株式会社 | 航空機及び航空機の制御方法 |
US10618645B2 (en) | 2015-08-25 | 2020-04-14 | Aerovironment, Inc. | Ganged servo flight control system for an unmanned aerial vehicle |
EP3653562A1 (de) * | 2018-11-19 | 2020-05-20 | B&R Industrial Automation GmbH | Verfahren und schwingungsregler zum ausregeln von schwingungen eines schwingfähigen technischen systems |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3201675A (en) * | 1962-11-01 | 1965-08-17 | Bendix Corp | Maximum command limiter device for an automatic flight control system |
US3390612A (en) * | 1965-07-06 | 1968-07-02 | Chandler Evans Inc | Dual stroke actuator |
US3429376A (en) * | 1966-10-18 | 1969-02-25 | Kurt H Hohenemser | Automatic control system for aircraft lifting rotor |
US3390614A (en) * | 1967-06-23 | 1968-07-02 | Newport News S & D Co | Electrohydraulic servocontrol system |
US3938762A (en) * | 1974-05-20 | 1976-02-17 | Textron, Inc. | Rotor blade force track sensing system and automatic span tracking system |
US4078750A (en) * | 1977-03-08 | 1978-03-14 | United Technologies Corporation | Speed-variable limits in fail-safe actuators |
US4133250A (en) * | 1977-06-22 | 1979-01-09 | Pneumo Corporation | Combined feedback control system |
US4094481A (en) * | 1977-06-30 | 1978-06-13 | Sperry Rand Corporation | Fail passive dual servo with continuous motor speed and acceleration and monitoring |
SE440129B (sv) * | 1979-06-20 | 1985-07-15 | Akermans Verkstad Ab | Anordning for att reducera kolvhastigheten i en cylinder, da kolven nermar sig endlegena |
US4420808A (en) * | 1980-04-01 | 1983-12-13 | United Technologies Corporation | Multi-axis force stick, self-trimmed aircraft flight control system |
US4305028A (en) * | 1980-04-04 | 1981-12-08 | Nordson Corporation | System for evaluating the capability of a work-performing robot to reproduce a programmed series of motions |
US4599698A (en) * | 1983-05-02 | 1986-07-08 | United Technologies Corporation | Aircraft trim actuator shutdown monitor system and method |
ATE48709T1 (de) * | 1983-06-03 | 1989-12-15 | Omron Tateisi Electronics Co | Zeitdiskret selbstanpassender ein/ausschaltregler. |
US4774651A (en) * | 1985-06-03 | 1988-09-27 | Vickers, Incorporated | Power transmission |
DE3612905C2 (de) * | 1986-04-17 | 1993-11-18 | Bosch Gmbh Robert | Verfahren zum Auslösen einer Schaltfunktion |
GB8629896D0 (en) * | 1986-12-15 | 1987-01-28 | Westland Plc | Helicopter flight control system |
US4866361A (en) * | 1988-05-05 | 1989-09-12 | The United States Of America As Represented By The Secretary Of The Navy | Actuator rate saturation compensator |
JPH0786776B2 (ja) * | 1988-11-12 | 1995-09-20 | 三田工業株式会社 | 移動体の制御装置 |
-
1991
- 1991-07-22 US US07/733,793 patent/US5224664A/en not_active Expired - Lifetime
-
1992
- 1992-07-09 EP EP92915770A patent/EP0595914B1/de not_active Expired - Lifetime
- 1992-07-09 ES ES92915770T patent/ES2083752T3/es not_active Expired - Lifetime
- 1992-07-09 JP JP5502854A patent/JPH06509198A/ja active Pending
- 1992-07-09 WO PCT/US1992/005742 patent/WO1993002405A1/en active IP Right Grant
- 1992-07-09 CA CA002113648A patent/CA2113648C/en not_active Expired - Fee Related
- 1992-07-09 AU AU23235/92A patent/AU657157B2/en not_active Ceased
- 1992-07-09 DE DE69206805T patent/DE69206805T2/de not_active Expired - Fee Related
- 1992-07-09 KR KR1019940700185A patent/KR100233345B1/ko not_active IP Right Cessation
- 1992-07-13 IL IL10248292A patent/IL102482A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
DE69206805T2 (de) | 1996-05-23 |
IL102482A0 (en) | 1993-02-21 |
CA2113648A1 (en) | 1993-02-04 |
AU657157B2 (en) | 1995-03-02 |
WO1993002405A1 (en) | 1993-02-04 |
DE69206805D1 (de) | 1996-01-25 |
US5224664A (en) | 1993-07-06 |
EP0595914B1 (de) | 1995-12-13 |
JPH06509198A (ja) | 1994-10-13 |
CA2113648C (en) | 2000-05-23 |
ES2083752T3 (es) | 1996-04-16 |
EP0595914A1 (de) | 1994-05-11 |
AU2323592A (en) | 1993-02-23 |
KR100233345B1 (ko) | 1999-12-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FF | Patent granted | ||
KB | Patent renewed | ||
KB | Patent renewed | ||
KB | Patent renewed | ||
MM9K | Patent not in force due to non-payment of renewal fees |