DE69304329D1 - Steuerungssystem zum koordinieren des umlenkens oder des beibehaltens des kurswinkels eines hubschraubers - Google Patents

Steuerungssystem zum koordinieren des umlenkens oder des beibehaltens des kurswinkels eines hubschraubers

Info

Publication number
DE69304329D1
DE69304329D1 DE69304329T DE69304329T DE69304329D1 DE 69304329 D1 DE69304329 D1 DE 69304329D1 DE 69304329 T DE69304329 T DE 69304329T DE 69304329 T DE69304329 T DE 69304329T DE 69304329 D1 DE69304329 D1 DE 69304329D1
Authority
DE
Germany
Prior art keywords
helicopter
coordinating
deviation
keeping
control system
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 - Fee Related
Application number
DE69304329T
Other languages
English (en)
Other versions
DE69304329T2 (de
Inventor
Porter Sherman
David Hetzler
Paul Weisser
Stuart Wright
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of DE69304329D1 publication Critical patent/DE69304329D1/de
Application granted granted Critical
Publication of DE69304329T2 publication Critical patent/DE69304329T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • G05D1/08—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
DE69304329T 1992-06-01 1993-05-24 Steuerungssystem zum koordinieren des umlenkens oder des beibehaltens des kurswinkels eines hubschraubers Expired - Fee Related DE69304329T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/891,624 US5299759A (en) 1992-06-01 1992-06-01 Helicopter turn coordination and heading hold mode control
PCT/US1993/004882 WO1993024873A1 (en) 1992-06-01 1993-05-24 Helicopter turn coordination and heading hold mode control

Publications (2)

Publication Number Publication Date
DE69304329D1 true DE69304329D1 (de) 1996-10-02
DE69304329T2 DE69304329T2 (de) 1997-01-16

Family

ID=25398548

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69304329T Expired - Fee Related DE69304329T2 (de) 1992-06-01 1993-05-24 Steuerungssystem zum koordinieren des umlenkens oder des beibehaltens des kurswinkels eines hubschraubers

Country Status (5)

Country Link
US (1) US5299759A (de)
EP (1) EP0643849B1 (de)
JP (1) JP3325024B2 (de)
DE (1) DE69304329T2 (de)
WO (1) WO1993024873A1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2734359B1 (fr) * 1995-05-17 1997-07-18 Eurocopter France Procede et dispositif pour determiner les configurations de vol d'un aeronef
US6205439B1 (en) * 1998-07-15 2001-03-20 Micron Technology, Inc. Optimization of simulation run-times based on fuzzy-controlled input values
DE202009001355U1 (de) * 2009-02-04 2009-05-20 RÖHR, Ulrich Modellflugkörpersteuer- und Empfangseinrichtung
US9304516B2 (en) 2011-01-14 2016-04-05 Textron Innovations Inc. Flight control laws for vertical flight path
DE102012003910A1 (de) 2011-04-15 2012-10-18 Ulrich Röhr System zur drahtlosen Steuerung eines RC-Modells, Sendeeinrichtung, Empfangseinrichtung sowie Verfahren
US9272780B2 (en) 2012-02-10 2016-03-01 Merlin Technology, Inc. Rotorcraft autopilot and methods
US9150308B2 (en) 2012-02-10 2015-10-06 Merlin Technology, Inc. Rotorcraft autopilot system, components and methods

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4067517A (en) * 1976-02-03 1978-01-10 United Technologies Corporation Automatic heading synchronization control system
US4003532A (en) * 1976-03-15 1977-01-18 United Technologies Corporation Heading hold logic
US4029271A (en) * 1976-04-07 1977-06-14 United Technologies Corporation Automatic approach to hover system
US4206891A (en) * 1978-10-26 1980-06-10 United Technologies Corporation Helicopter pedal feel force proportional to side slip
US4300200A (en) * 1978-12-01 1981-11-10 Westland Aircraft Limited Helicopter airspeed indicating system
US4484283A (en) * 1981-03-30 1984-11-20 United Technologies Corporation Aircraft roll-yaw fault protocols
US4645141A (en) * 1984-05-23 1987-02-24 Rockwell International Corporation Automatic flight control system
JPH0698903B2 (ja) * 1986-08-06 1994-12-07 本田技研工業株式会社 車両走行制御装置
JPS63251805A (ja) * 1987-04-08 1988-10-19 Hitachi Ltd エンジンの状態別適応制御方式
US5036936A (en) * 1988-09-20 1991-08-06 Mitsubishi Jidosha Kogyo Kabushiki Kaisha Cruise control device for motor vehicles
US5076517A (en) * 1989-08-14 1991-12-31 United Technologies Corporation Programmable, linear collective control system for a helicopter
US5195039A (en) * 1990-05-03 1993-03-16 United Technologies Corporation Hover position hold system for rotary winged aircraft

Also Published As

Publication number Publication date
US5299759A (en) 1994-04-05
DE69304329T2 (de) 1997-01-16
WO1993024873A1 (en) 1993-12-09
JP3325024B2 (ja) 2002-09-17
EP0643849A1 (de) 1995-03-22
EP0643849B1 (de) 1996-08-28
JPH07507255A (ja) 1995-08-10

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee