IT8220490A0 - Sistema azionatore ad impulsi per aeromobili. - Google Patents

Sistema azionatore ad impulsi per aeromobili.

Info

Publication number
IT8220490A0
IT8220490A0 IT8220490A IT2049082A IT8220490A0 IT 8220490 A0 IT8220490 A0 IT 8220490A0 IT 8220490 A IT8220490 A IT 8220490A IT 2049082 A IT2049082 A IT 2049082A IT 8220490 A0 IT8220490 A0 IT 8220490A0
Authority
IT
Italy
Prior art keywords
aircraft
drive system
pulse drive
pulse
drive
Prior art date
Application number
IT8220490A
Other languages
English (en)
Other versions
IT8220490A1 (it
IT1151536B (it
Inventor
Stuart Cammett Wright
Don Luisi Adams
William Christina Fischer
David John Verzella
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 IT8220490A0 publication Critical patent/IT8220490A0/it
Publication of IT8220490A1 publication Critical patent/IT8220490A1/it
Application granted granted Critical
Publication of IT1151536B publication Critical patent/IT1151536B/it

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
    • G05D1/08—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
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0833—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using limited authority control

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Security & Cryptography (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
IT20490/82A 1981-03-30 1982-03-30 Sistema azionatore ad impulsi per aeromobili IT1151536B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/249,300 US4387432A (en) 1981-03-30 1981-03-30 Pulsed aircraft actuator

Publications (3)

Publication Number Publication Date
IT8220490A0 true IT8220490A0 (it) 1982-03-30
IT8220490A1 IT8220490A1 (it) 1983-09-30
IT1151536B IT1151536B (it) 1986-12-24

Family

ID=22942880

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20490/82A IT1151536B (it) 1981-03-30 1982-03-30 Sistema azionatore ad impulsi per aeromobili

Country Status (6)

Country Link
US (1) US4387432A (it)
JP (1) JPH0641280B2 (it)
BR (1) BR8201663A (it)
DE (1) DE3210868A1 (it)
GB (1) GB2095870B (it)
IT (1) IT1151536B (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4563743A (en) * 1983-02-22 1986-01-07 United Technologies Corporation Maneuver-force gradient system
GB2135796B (en) * 1983-02-28 1986-07-09 United Technologies Corp Variable trim-engagement system
US4594714A (en) * 1983-05-02 1986-06-10 United Technologies Corporation Dual-actuator monitor
US4592055A (en) * 1983-05-02 1986-05-27 United Technologies Corporation Outer-loop monitor for aircraft automatic flight control system
RU2117324C1 (ru) * 1997-04-29 1998-08-10 Конструкторское бюро приборостроения Автоколебательный автопилот управляемого снаряда
US6240246B1 (en) 1998-10-30 2001-05-29 Alliedsignal, Inc. Anti-resonance mixing filter
US7081729B2 (en) * 2004-03-23 2006-07-25 The Boeing Company Variable-structure diagnostics approach achieving optimized low-frequency data sampling for EMA motoring subsystem
US20090302173A1 (en) * 2006-09-01 2009-12-10 Science Applications International Corporation Automatic flight control systems
WO2008051193A2 (en) * 2006-09-01 2008-05-02 Science Applications International Corporation Automatic flight control systems
US9272780B2 (en) 2012-02-10 2016-03-01 Merlin Technology, Inc. Rotorcraft autopilot and methods
CN102654773B (zh) * 2012-05-15 2015-03-04 北京航空航天大学 一种基于zvdd和pwm混合输入成型器的挠性航天器控制方法
US9856017B2 (en) * 2013-06-11 2018-01-02 Bell Helicopter Textron Inc. Torque based method of limiting vertical axis augmentation
DE102013107268B4 (de) * 2013-07-09 2017-01-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Vorrichtung zur Kompensation einer Luftresonanz bei einem Hubschrauber
FR3082637B1 (fr) * 2018-06-14 2021-10-29 Thales Sa Dispositif et procede de conversion d'un signal de consigne de guidage en un signal de commande pour systeme avionique, systeme d'aide au pilotage et programme d'ordinateur associes

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5160397A (en) * 1974-11-22 1976-05-26 Kawasaki Heavy Ind Ltd Kaitenyokukokuki niokeru jidohikoseigyosochi
CA1050633A (en) * 1974-12-19 1979-03-13 Ronald J. Miller Semi-automatic flight control system utilizing limited authority stabilization system
US4029271A (en) * 1976-04-07 1977-06-14 United Technologies Corporation Automatic approach to hover system
US4078750A (en) * 1977-03-08 1978-03-14 United Technologies Corporation Speed-variable limits in fail-safe actuators
US4213584A (en) * 1978-10-04 1980-07-22 United Technologies Corporation Helicopter hover stability and cruise gust effect alleviation
US4279391A (en) * 1979-01-24 1981-07-21 United Technologies Corporation Desensitizing helicopter control response to inadvertent pilot inputs
US4382283A (en) * 1980-08-08 1983-05-03 United Technologies Corporation Helicopter attitude and airspeed acquisition and retention system

Also Published As

Publication number Publication date
BR8201663A (pt) 1983-02-16
JPH0641280B2 (ja) 1994-06-01
IT8220490A1 (it) 1983-09-30
GB2095870A (en) 1982-10-06
JPS57178999A (en) 1982-11-04
DE3210868A1 (de) 1982-10-21
GB2095870B (en) 1984-08-01
IT1151536B (it) 1986-12-24
DE3210868C2 (it) 1992-12-10
US4387432A (en) 1983-06-07

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970228