IL113318A - Turn coordination inhibit apparatus for aircraft control system - Google Patents

Turn coordination inhibit apparatus for aircraft control system

Info

Publication number
IL113318A
IL113318A IL11331895A IL11331895A IL113318A IL 113318 A IL113318 A IL 113318A IL 11331895 A IL11331895 A IL 11331895A IL 11331895 A IL11331895 A IL 11331895A IL 113318 A IL113318 A IL 113318A
Authority
IL
Israel
Prior art keywords
turn coordination
inhibit
magnitude
signal
yaw
Prior art date
Application number
IL11331895A
Other languages
English (en)
Other versions
IL113318A0 (en
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 IL113318A0 publication Critical patent/IL113318A0/xx
Publication of IL113318A publication Critical patent/IL113318A/en

Links

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
    • G05D1/40—Control within particular dimensions
    • G05D1/49—Control of attitude, i.e. control of roll, pitch or yaw
    • 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2109/00—Types of controlled vehicles
    • G05D2109/20—Aircraft, e.g. drones
    • G05D2109/25—Rotorcrafts

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Retarders (AREA)
  • Control Of Velocity Or Acceleration (AREA)
  • Traffic Control Systems (AREA)
IL11331895A 1994-05-03 1995-04-11 Turn coordination inhibit apparatus for aircraft control system IL113318A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/237,540 US5553817A (en) 1994-05-03 1994-05-03 Turn coordination inhibit for rotary wing aircraft control system

Publications (2)

Publication Number Publication Date
IL113318A0 IL113318A0 (en) 1995-07-31
IL113318A true IL113318A (en) 1998-10-30

Family

ID=22894175

Family Applications (1)

Application Number Title Priority Date Filing Date
IL11331895A IL113318A (en) 1994-05-03 1995-04-11 Turn coordination inhibit apparatus for aircraft control system

Country Status (10)

Country Link
US (1) US5553817A (ja)
EP (1) EP0759196B1 (ja)
JP (1) JPH09512762A (ja)
KR (1) KR100291877B1 (ja)
AU (1) AU681279B2 (ja)
CA (1) CA2189455C (ja)
DE (1) DE69504497T2 (ja)
ES (1) ES2121370T3 (ja)
IL (1) IL113318A (ja)
WO (1) WO1995030181A1 (ja)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6648269B2 (en) 2001-12-10 2003-11-18 Sikorsky Aircraft Corporation Trim augmentation system for a rotary wing aircraft
US7930074B2 (en) * 2007-03-19 2011-04-19 Sikorsky Aircraft Corporation Vertical speed and flight path command module for displacement collective utilizing tactile cueing and tactile feedback
CA2824932C (en) 2011-01-14 2016-03-22 Bell Helicopter Textron Inc. Flight control laws for vertical flight path control
US9098090B2 (en) * 2011-03-29 2015-08-04 Textron Innovations Inc. Flight control laws for full envelope banked turns
EP2673681B1 (en) * 2011-03-30 2016-09-07 Bell Helicopter Textron Inc. Flight control laws for constant vector flat turns
JP5791460B2 (ja) * 2011-10-21 2015-10-07 三菱重工業株式会社 航空機及び航空機の制御方法
US8718841B2 (en) 2012-02-14 2014-05-06 Sikorsky Aircraft Corporation Method and system for providing sideslip envelope protection
US9651948B2 (en) * 2015-09-14 2017-05-16 The Boeing Company Roll attitude-dependent roll rate limit

Family Cites Families (10)

* 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
US4206891A (en) * 1978-10-26 1980-06-10 United Technologies Corporation Helicopter pedal feel force proportional to side slip
US4371939A (en) * 1981-03-30 1983-02-01 United Technologies Corporation Roll attitude inhibit of aircraft coordinated turn disengagement
US5213283A (en) * 1991-08-28 1993-05-25 United Technologies Corporation Low speed turn coordination for rotary wing aircraft
US5141177A (en) * 1991-08-28 1992-08-25 United Technologies Corporation Model following control system
US5178307A (en) * 1991-08-28 1993-01-12 United Technologies Corporation High speed yaw control system for rotary wing aircraft
US5222691A (en) * 1991-08-28 1993-06-29 United Technologies Corporation Automatic turn coordination trim control for rotary wing aircraft
US5238203A (en) * 1991-08-28 1993-08-24 United Technologies Corporation High speed turn coordination for rotary wing aircraft
US5195700A (en) * 1991-08-28 1993-03-23 United Technologies Corporation Low speed model following velocity command system for rotary wing aircraft
US5263662A (en) * 1992-05-19 1993-11-23 United Technologies Corporation Helicopter integrated fire and flight control system having turn coordination control

Also Published As

Publication number Publication date
CA2189455A1 (en) 1995-11-09
US5553817A (en) 1996-09-10
JPH09512762A (ja) 1997-12-22
WO1995030181A1 (en) 1995-11-09
KR970703007A (ko) 1997-06-10
EP0759196B1 (en) 1998-09-02
AU681279B2 (en) 1997-08-21
IL113318A0 (en) 1995-07-31
EP0759196A1 (en) 1997-02-26
ES2121370T3 (es) 1998-11-16
KR100291877B1 (ko) 2001-06-01
DE69504497D1 (de) 1998-10-08
AU2246895A (en) 1995-11-29
DE69504497T2 (de) 1999-01-28
CA2189455C (en) 2003-02-11

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Legal Events

Date Code Title Description
FF Patent granted
KB Patent renewed
MM9K Patent not in force due to non-payment of renewal fees