GB1315506A - Marine autopilot systems - Google Patents
Marine autopilot systemsInfo
- Publication number
- GB1315506A GB1315506A GB4157670A GB4157670A GB1315506A GB 1315506 A GB1315506 A GB 1315506A GB 4157670 A GB4157670 A GB 4157670A GB 4157670 A GB4157670 A GB 4157670A GB 1315506 A GB1315506 A GB 1315506A
- Authority
- GB
- United Kingdom
- Prior art keywords
- heading
- difference
- relays
- actual
- aug
- 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
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/02—Control of position or course in two dimensions
- G05D1/0206—Control of position or course in two dimensions specially adapted to water vehicles
Abstract
1315506 Automatic steering control TOKYO KEIKI K K 28 Aug 1970 [30 Aug 1969] 41576/70 Heading G3R A marine auto-pilot system has provision for course changes to be initiated manually, such changes then being carried out automatically, at least one of the constants and functions of the auto-pilot system being altered and others eliminated upon generation of the manual initiating means. As described, a signal from a compass corresponding to the heading of a ship is compared with a signal representing a desired heading so that any difference is effective through a dead band device, a PID controller, a limiter, and a follow-up servo-system operating the rudder to correct the heading. An alarm is operated if the difference becomes excessive. In Fig. 3, to set the heading, a knob 24 is depressed to engage a clutch 27 and the input to a differential gear 28 rotated. The differential gear compares the set heading with the actual heading # transmitted from the gyro-compass through a synchro transmission 21, 22 so that any difference is effective through a synchro 23 to actuate the steering control system 30. Operation of knob 24 to change the heading causes actuation of a switch 26 so that a transistor multi-vibrator 32 is triggered to energize electro-magnetic or transistor relays 34 for a limited time period duringÀwhich the heading is being charged. Relays 34 may remove the dead band and limiter devices and the integral control term, alter the time constant of the differential control term and disable the alarm. A resistor 33 is adjusted in dependence on the magnitude of the difference between the set and actual heading so that the response of the control system is altered by relays 34 for a corresponding period. Modifications are described in which the alteration in response is initiated when the difference between the set and actual heading exceeds a predetermined value.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP44068794A JPS5030915B1 (en) | 1969-08-30 | 1969-08-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1315506A true GB1315506A (en) | 1973-05-02 |
Family
ID=13383965
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4157670A Expired GB1315506A (en) | 1969-08-30 | 1970-08-28 | Marine autopilot systems |
Country Status (6)
Country | Link |
---|---|
US (1) | US3696282A (en) |
JP (1) | JPS5030915B1 (en) |
DE (1) | DE2042753C3 (en) |
DK (1) | DK133025C (en) |
GB (1) | GB1315506A (en) |
SE (1) | SE366705B (en) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3895280A (en) * | 1972-03-14 | 1975-07-15 | Foxboro Co | Electronic controller with remote tuning |
JPS5247231B2 (en) * | 1972-05-27 | 1977-12-01 | ||
US3867712A (en) * | 1972-06-28 | 1975-02-18 | Honeywell Inc | Adaptive filter |
US3838656A (en) * | 1972-08-21 | 1974-10-01 | Safe Flight Instrument | Marine automatic pilot rudder motor control system |
GB1416401A (en) * | 1973-03-06 | 1975-12-03 | Rolls Royce | Control systems |
US3946691A (en) * | 1973-10-17 | 1976-03-30 | Metal Marine Pilot, Inc. | Autopilot employing improved hall-effect direction sensor |
US3939328A (en) * | 1973-11-06 | 1976-02-17 | Westinghouse Electric Corporation | Control system with adaptive process controllers especially adapted for electric power plant operation |
US3857353A (en) * | 1974-02-05 | 1974-12-31 | G Mounce | Sailing vessel self-steering system |
US4040374A (en) * | 1974-03-18 | 1977-08-09 | Safe Flight Instrument Corporation | Automatic pilot for a sailboat |
US3952681A (en) * | 1974-04-01 | 1976-04-27 | Tucker Systems, Inc. | Automatic steering system for vessels with a wireless remote control and course change capability |
US4070609A (en) * | 1975-01-02 | 1978-01-24 | Barber-Colman Company | Automatic control system |
JPS5195384A (en) * | 1975-02-17 | 1976-08-20 | ||
US3998409A (en) * | 1975-03-11 | 1976-12-21 | Rca Corporation | Minimization of spacecraft attitude error due to wheel speed reversal |
US3999729A (en) * | 1975-03-20 | 1976-12-28 | Rca Corporation | Backup wheel for a three axis reaction wheel spacecraft |
US4275676A (en) * | 1977-03-11 | 1981-06-30 | Nippon Gakki Seizo Kabushiki Kaisha | Auto-steering system |
JPS60277B2 (en) * | 1977-12-28 | 1985-01-07 | 株式会社トキメック | Marine automatic steering system |
US4346433A (en) * | 1980-03-11 | 1982-08-24 | Phillips Petroleum Company | Process control |
US4420808A (en) * | 1980-04-01 | 1983-12-13 | United Technologies Corporation | Multi-axis force stick, self-trimmed aircraft flight control system |
US4319173A (en) * | 1980-06-12 | 1982-03-09 | Rockwell International Corporation | Dual polarity fast discharge integrator apparatus |
US4342274A (en) * | 1980-08-11 | 1982-08-03 | Sperry Corporation | Steering failure alarm |
FR2500988A1 (en) * | 1981-03-06 | 1982-09-10 | Lestradet M C J | VEHICLE GUIDING DEVICE, IN PARTICULAR AGRICULTURAL ENGINE |
DE3212950C1 (en) * | 1982-04-07 | 1983-10-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Flight control, especially for a helicopter |
US4538230A (en) * | 1982-10-29 | 1985-08-27 | Conoco Inc. | Method and apparatus for controlling altitude |
GB8425442D0 (en) * | 1984-10-09 | 1984-11-14 | Devon County Council Burns R | Automatic vehicle control method |
US5034895A (en) * | 1990-01-03 | 1991-07-23 | Sperry Marine Inc. | Enhanced performance bias integrator for marine automatic pilot system |
SE509982C2 (en) * | 1997-08-13 | 1999-03-29 | Saab Ab | Method and device for phase compensation in a vehicle control system |
JP4178790B2 (en) * | 2001-12-26 | 2008-11-12 | スズキ株式会社 | Outboard engine reset device |
JP3683890B2 (en) * | 2003-03-31 | 2005-08-17 | 財団法人ファジィシステム研究所 | Control device and method for ships, etc. |
JP3677274B2 (en) * | 2003-03-31 | 2005-07-27 | 財団法人ファジィシステム研究所 | Control apparatus and method |
US7034492B2 (en) * | 2003-10-28 | 2006-04-25 | Ge Medical Systems Global Technology Company, Llc | Methods and systems for reducing unintentional collisions |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3301510A (en) * | 1963-11-01 | 1967-01-31 | Thiokol Chemical Corp | Method and apparatus for gage simulation in automatic control systems |
US3510737A (en) * | 1964-12-21 | 1970-05-05 | Honeywell Inc | Servomechanism including paralleled "lead-lag" channels and means to disable lag channel responsive to excessive rate |
US3431475A (en) * | 1965-08-18 | 1969-03-04 | Sperry Rand Corp | Solid state servo system including a unique d.c. control triggering a.c. power to the servomotor |
US3280781A (en) * | 1965-09-27 | 1966-10-25 | Bunker Ramo | Auto-pilot system |
US3505577A (en) * | 1966-04-13 | 1970-04-07 | Tokyo Keiki Kk | Adaptive control for ship steering whereby system is less sensitive in rough sea |
US3493825A (en) * | 1967-12-19 | 1970-02-03 | Bestran Corp | Flat capacitor |
US3517285A (en) * | 1968-09-04 | 1970-06-23 | Anschuetz & Co Gmbh | Electrical automatic pilot for rudder-controlled vehicles,particularly for ships |
US3571684A (en) * | 1969-08-12 | 1971-03-23 | Decca Ltd | Rudder positioning unit for the steering systems of ships |
-
1969
- 1969-08-30 JP JP44068794A patent/JPS5030915B1/ja active Pending
-
1970
- 1970-08-26 US US66939A patent/US3696282A/en not_active Expired - Lifetime
- 1970-08-28 DE DE2042753A patent/DE2042753C3/en not_active Expired
- 1970-08-28 GB GB4157670A patent/GB1315506A/en not_active Expired
- 1970-08-28 DK DK442570A patent/DK133025C/en active
- 1970-12-28 SE SE11695/70*[A patent/SE366705B/xx unknown
Also Published As
Publication number | Publication date |
---|---|
DK133025C (en) | 1976-08-30 |
SE366705B (en) | 1974-05-06 |
DK133025B (en) | 1976-03-08 |
DE2042753B2 (en) | 1974-04-18 |
DE2042753A1 (en) | 1971-04-15 |
US3696282A (en) | 1972-10-03 |
DE2042753C3 (en) | 1974-11-21 |
JPS5030915B1 (en) | 1975-10-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |