GB2000609A - Feedback Control Systems - Google Patents
Feedback Control SystemsInfo
- Publication number
- GB2000609A GB2000609A GB7827946A GB7827946A GB2000609A GB 2000609 A GB2000609 A GB 2000609A GB 7827946 A GB7827946 A GB 7827946A GB 7827946 A GB7827946 A GB 7827946A GB 2000609 A GB2000609 A GB 2000609A
- Authority
- GB
- United Kingdom
- Prior art keywords
- control
- processor
- signal
- feedback
- components
- 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.)
- Granted
Links
- 238000006073 displacement reaction Methods 0.000 abstract 2
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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
-
- 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
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B9/00—Safety arrangements
- G05B9/02—Safety arrangements electric
- G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
-
- 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
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
A control system for controlling displacement of the aerodynamic control-surfaces (10) of an aircraft in response to movement of the pilot's control column (18). The system includes a first processor (16) that is supplied with input signals from the pilot's control column (18) and also with predominantly lower-frequency components of feedback signals from the control- surfaces (10). The first processor (16) derives an intermediate signal from the input signal and the feedback signal components by digital processing and supplies this intermediate signal to a second processor (25) which also receives the predominantly higher-frequency components of the feedback signal. The second processor (25) derives an output signal from the intermediate signal and the feedback signal components by analogue processing and supplies this to an actuator (14) for controlling displacement of the control-surfaces. The system may include a plurality of first and second processors arranged to provide a degree of redundancy. <IMAGE>
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7827946A GB2000609B (en) | 1977-07-04 | 1978-06-27 | Control systems |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2793377 | 1977-07-04 | ||
GB7827946A GB2000609B (en) | 1977-07-04 | 1978-06-27 | Control systems |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2000609A true GB2000609A (en) | 1979-01-10 |
GB2000609B GB2000609B (en) | 1982-01-06 |
Family
ID=26259073
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7827946A Expired GB2000609B (en) | 1977-07-04 | 1978-06-27 | Control systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2000609B (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0031619A2 (en) * | 1979-12-26 | 1981-07-08 | The Boeing Company | Vertical flight path steering system for aircraft |
EP0041701A2 (en) * | 1980-06-09 | 1981-12-16 | Hitachi, Ltd. | Multiple digital controller system |
EP0050168A2 (en) * | 1980-10-03 | 1982-04-28 | Fanuc Ltd. | A position control system for a numerical-controlled machine tool |
EP0058861A1 (en) * | 1981-02-17 | 1982-09-01 | Bell Helicopter Textron Inc. | Multiple loop control system |
EP0074862A1 (en) * | 1977-07-04 | 1983-03-23 | Fischer & Porter Company | Auxiliary channel for direct digital control system |
EP0110885A1 (en) * | 1982-06-16 | 1984-06-20 | Boeing Co | Autopilot flight director system. |
US4542679A (en) * | 1981-02-17 | 1985-09-24 | Textron Inc. | Multiple loop control system |
EP0653690A1 (en) * | 1993-10-20 | 1995-05-17 | United Technologies Corporation | Dual control with dual sensor averaging and substitution |
EP1840681A1 (en) * | 2006-03-29 | 2007-10-03 | Integrated Dynamics Engineering GmbH | Method and device for controlling vibration isolation systems |
WO2011072362A1 (en) | 2009-12-18 | 2011-06-23 | National Research Council Of Canada | Response mode for control system of piloted craft |
-
1978
- 1978-06-27 GB GB7827946A patent/GB2000609B/en not_active Expired
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0074862A1 (en) * | 1977-07-04 | 1983-03-23 | Fischer & Porter Company | Auxiliary channel for direct digital control system |
EP0031619A3 (en) * | 1979-12-26 | 1981-07-22 | The Boeing Company | Vertical flight path steering system for aircraft |
EP0031619A2 (en) * | 1979-12-26 | 1981-07-08 | The Boeing Company | Vertical flight path steering system for aircraft |
EP0041701A2 (en) * | 1980-06-09 | 1981-12-16 | Hitachi, Ltd. | Multiple digital controller system |
EP0041701A3 (en) * | 1980-06-09 | 1982-12-08 | Hitachi, Ltd. | Multiple digital controller system |
EP0050168A2 (en) * | 1980-10-03 | 1982-04-28 | Fanuc Ltd. | A position control system for a numerical-controlled machine tool |
EP0050168A3 (en) * | 1980-10-03 | 1982-05-26 | Fanuc Ltd. | A position control system for a numerical-controlled machine tool |
US4542679A (en) * | 1981-02-17 | 1985-09-24 | Textron Inc. | Multiple loop control system |
EP0058861A1 (en) * | 1981-02-17 | 1982-09-01 | Bell Helicopter Textron Inc. | Multiple loop control system |
EP0110885A4 (en) * | 1982-06-16 | 1986-02-13 | Boeing Co | Autopilot flight director system. |
EP0110885A1 (en) * | 1982-06-16 | 1984-06-20 | Boeing Co | Autopilot flight director system. |
EP0653690A1 (en) * | 1993-10-20 | 1995-05-17 | United Technologies Corporation | Dual control with dual sensor averaging and substitution |
EP1840681A1 (en) * | 2006-03-29 | 2007-10-03 | Integrated Dynamics Engineering GmbH | Method and device for controlling vibration isolation systems |
JP2007265414A (en) * | 2006-03-29 | 2007-10-11 | Integrated Dynamics Engineering Gmbh | Method and device for regulating vibration isolation system |
US7715948B2 (en) | 2006-03-29 | 2010-05-11 | Integrated Dynamics Engineering Gmbh | Method and apparatus for regulating vibration isolation systems |
WO2011072362A1 (en) | 2009-12-18 | 2011-06-23 | National Research Council Of Canada | Response mode for control system of piloted craft |
EP2512916A1 (en) * | 2009-12-18 | 2012-10-24 | National Research Council of Canada | Response mode for control system of piloted craft |
JP2013514215A (en) * | 2009-12-18 | 2013-04-25 | ナショナル リサーチ カウンシル オブ カナダ | Response mode for control system of maneuvered craft |
EP2512916A4 (en) * | 2009-12-18 | 2013-07-10 | Ca Nat Research Council | Response mode for control system of piloted craft |
US8688295B2 (en) | 2009-12-18 | 2014-04-01 | National Research Council Of Canada | Response mode for control system of piloted craft |
Also Published As
Publication number | Publication date |
---|---|
GB2000609B (en) | 1982-01-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2000609A (en) | Feedback Control Systems | |
KR930007055A (en) | Servo motor controller | |
SE8301026D0 (en) | CLUTCH DEVICE FOR CONTROL OF THE MOVEMENT OF AN ADJUSTMENT DEVICE, IN PARTICULAR A PATIENT CHAIR | |
US3508512A (en) | Automatic system for dynamically anchoring a floating installation | |
ES2111127T3 (en) | PASSIVE AIRCRAFT CONTROL SYSTEM. | |
US4279391A (en) | Desensitizing helicopter control response to inadvertent pilot inputs | |
EP0371585A3 (en) | Controlling nuclear reactor coolant systems | |
GB1178673A (en) | Improvements in and relating to the Control of Aircraft | |
DE69130112D1 (en) | SYSTEM FOR ACTIVE VIBRATION CONTROL | |
US2852212A (en) | Automatic and manual control apparatus for aircraft | |
ZA847567B (en) | Method of and apparatus for operating multi-processor control computer units | |
Smith et al. | Effect of control system delays on fighter flying qualities | |
Gibson | Handling qualities for unstable combat aircraft | |
SE8402645L (en) | SIGNAL DISEASE DEVICE FOR THE DISABLED | |
US3128968A (en) | Aircraft control servo apparatus having signal memorizing means | |
NL7701000A (en) | Flight simulator with elements coupled to servo system - has computer using flight conditions and element characteristics to convert to control signals | |
GB1337423A (en) | Actuators particularly for aircraft power control systems | |
GB803574A (en) | Control systems for aircraft | |
GB803576A (en) | Control systems for aircraft | |
Watanabe et al. | NAL flight simulator real-time computer systems | |
GB1148354A (en) | Improvements in or relating to control apparatus for use in aircraft | |
JPS5762424A (en) | Follow-up steering signal generator | |
Pineiro et al. | Parameter-adaptive model-following for in-flight simulation | |
GB1326637A (en) | Automatic pilot for ships | |
GB1271390A (en) | Control for fog simulator effects |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
746 | Register noted 'licences of right' (sect. 46/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19930627 |