IT1206557B - Sistema di controllo di stabilita'per aeroplani - Google Patents

Sistema di controllo di stabilita'per aeroplani

Info

Publication number
IT1206557B
IT1206557B IT7852269A IT5226978A IT1206557B IT 1206557 B IT1206557 B IT 1206557B IT 7852269 A IT7852269 A IT 7852269A IT 5226978 A IT5226978 A IT 5226978A IT 1206557 B IT1206557 B IT 1206557B
Authority
IT
Italy
Prior art keywords
airplanes
control system
stability control
stability
control
Prior art date
Application number
IT7852269A
Other languages
English (en)
Other versions
IT7852269A0 (it
Original Assignee
Sperry Rand 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 Sperry Rand Corp filed Critical Sperry Rand Corp
Publication of IT7852269A0 publication Critical patent/IT7852269A0/it
Application granted granted Critical
Publication of IT1206557B publication Critical patent/IT1206557B/it

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0607Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0615Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind

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)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
IT7852269A 1977-12-12 1978-12-12 Sistema di controllo di stabilita'per aeroplani IT1206557B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/859,410 US4171115A (en) 1977-12-12 1977-12-12 Stability augmentation system for relaxed static stability aircraft

Publications (2)

Publication Number Publication Date
IT7852269A0 IT7852269A0 (it) 1978-12-12
IT1206557B true IT1206557B (it) 1989-04-27

Family

ID=25330855

Family Applications (1)

Application Number Title Priority Date Filing Date
IT7852269A IT1206557B (it) 1977-12-12 1978-12-12 Sistema di controllo di stabilita'per aeroplani

Country Status (7)

Country Link
US (1) US4171115A (it)
JP (1) JPS5488600A (it)
CA (1) CA1111938A (it)
DE (1) DE2853612A1 (it)
FR (1) FR2411440A1 (it)
GB (1) GB2009970B (it)
IT (1) IT1206557B (it)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4562546A (en) * 1983-01-13 1985-12-31 Rockwell International Corporation Stability augmentation system for a forward swept wing aircraft
US4703697A (en) * 1984-04-19 1987-11-03 Bell George S Transportation system
US4536689A (en) * 1984-05-17 1985-08-20 Sperry Corporation Servomotor feedback fault detector
DE3431597A1 (de) * 1984-08-28 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur verbesserung der laengssteuerstabilitaet von luftfahrzeugen
JP2569130Y2 (ja) * 1991-03-29 1998-04-22 株式会社大井製作所 自動変速機のシフトレバー装置
JPH0557510U (ja) * 1991-12-28 1993-07-30 デルタ工業株式会社 自動車用チェンジレバーのシフトロック装置
US5631830A (en) 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
US5590850A (en) * 1995-06-05 1997-01-07 Hughes Missile Systems Company Blended missile autopilot
US5880680A (en) * 1996-12-06 1999-03-09 The Charles Machine Works, Inc. Apparatus and method for determining boring direction when boring underground
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
FR2838101B1 (fr) * 2002-04-08 2004-12-17 Airbus France Aeronef a commandes de vol electriques, pourvu d'un fuselage susceptible de se deformer et de vibrer
US7272473B2 (en) * 2004-09-17 2007-09-18 The Boeing Company Methods and systems for analyzing system operator coupling susceptibility
FR2909462B1 (fr) * 2006-12-05 2008-12-26 Airbus France Sas Procede et dispositif de controle actif du tangage d'un avion.
US7970498B2 (en) * 2007-06-01 2011-06-28 Sikorsky Aircraft Corporation Model based sensor system for loads aware control laws
TWI374257B (en) * 2008-04-29 2012-10-11 Ind Tech Res Inst Method for modifying navigation information and navigation apparatus using the same
JP7097052B2 (ja) * 2018-04-04 2022-07-07 国立研究開発法人宇宙航空研究開発機構 飛行機の突風応答軽減システム及び飛行機の突風応答軽減方法
CN110667832B (zh) * 2019-10-01 2022-11-15 西安爱生技术集团公司 一种十六旋翼飞行器垂起俯仰姿态梯度控制方法
DE102020202156A1 (de) * 2020-02-19 2021-08-19 Volkswagen Aktiengesellschaft Ermitteln von Wankgeschwindigkeit und Nickgeschwindigkeit aus Winkelgrößen und Beschleunigungsgrößen eines Kraftfahrzeugs
CN114924581B (zh) * 2022-07-21 2022-12-13 成都飞机工业(集团)有限责任公司 一种单余度无人机俯仰角失效的判定方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2487793A (en) * 1946-12-18 1949-11-15 Sperry Corp Object controlling electric motor system
US2808999A (en) * 1949-05-07 1957-10-08 Sperry Rand Corp Automatic flight control apparatus
US3007656A (en) * 1956-03-15 1961-11-07 Sperry Rand Corp Aircraft automatic pilots
US3100861A (en) * 1960-12-23 1963-08-13 Sperry Rand Corp Fail-safe control systems for aircraft
US3752420A (en) * 1971-01-04 1973-08-14 Sperry Rand Corp Augmented washout circuit for use in automatic pilots

Also Published As

Publication number Publication date
FR2411440B1 (it) 1983-12-23
CA1111938A (en) 1981-11-03
GB2009970A (en) 1979-06-20
JPS5488600A (en) 1979-07-13
US4171115A (en) 1979-10-16
JPH02240B2 (it) 1990-01-05
DE2853612A1 (de) 1979-06-21
IT7852269A0 (it) 1978-12-12
GB2009970B (en) 1982-03-31
FR2411440A1 (fr) 1979-07-06

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