SE8303431L - Metsystem for flygplan - Google Patents

Metsystem for flygplan

Info

Publication number
SE8303431L
SE8303431L SE8303431A SE8303431A SE8303431L SE 8303431 L SE8303431 L SE 8303431L SE 8303431 A SE8303431 A SE 8303431A SE 8303431 A SE8303431 A SE 8303431A SE 8303431 L SE8303431 L SE 8303431L
Authority
SE
Sweden
Prior art keywords
aircraft
center
gravity
location
signal
Prior art date
Application number
SE8303431A
Other languages
English (en)
Swedish (sv)
Other versions
SE8303431D0 (sv
Inventor
J H Glover
Original Assignee
Sundstrand Data Control
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 Sundstrand Data Control filed Critical Sundstrand Data Control
Publication of SE8303431D0 publication Critical patent/SE8303431D0/xx
Publication of SE8303431L publication Critical patent/SE8303431L/

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/12—Static balancing; Determining position of centre of gravity
    • G01M1/122—Determining position of centre of gravity
    • G01M1/125—Determining position of centre of gravity of aircraft
    • G01M1/127—Determining position of centre of gravity of aircraft during the flight

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Balance (AREA)
  • Navigation (AREA)
SE8303431A 1982-06-18 1983-06-15 Metsystem for flygplan SE8303431L (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/389,803 US4545019A (en) 1982-06-18 1982-06-18 Aircraft in-flight center of gravity measuring system

Publications (2)

Publication Number Publication Date
SE8303431D0 SE8303431D0 (sv) 1983-06-15
SE8303431L true SE8303431L (sv) 1983-12-19

Family

ID=23539790

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8303431A SE8303431L (sv) 1982-06-18 1983-06-15 Metsystem for flygplan

Country Status (12)

Country Link
US (1) US4545019A ( )
JP (1) JPS5910827A ( )
AU (1) AU544746B2 ( )
CA (1) CA1211567A ( )
DE (1) DE3321922A1 ( )
FR (1) FR2528978B1 ( )
GB (1) GB2122355B ( )
IL (1) IL68915A ( )
IT (1) IT1201068B ( )
NL (1) NL8302177A ( )
NZ (1) NZ204481A ( )
SE (1) SE8303431L ( )

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2609546B1 (fr) * 1987-01-08 1991-01-04 Aerospatiale Procede et systeme pour la determination de la position longitudinale du centre de gravite d'un aeronef pourvu d'un empennage horizontal reglable
FR2609545B1 (fr) * 1987-01-08 1991-01-04 Aerospatiale Procede et systeme pour la determination de la position longitudinale du centre de gravite d'un aeronef pourvu d'un empennage horizontal reglable et application a la surveillance dudit centre de gravite au voisinage du foyer de l'aeronef
US5034896A (en) * 1990-01-26 1991-07-23 The Boeing Company Method and apparatus for real time estimation of aircraft center of gravity
US5136513A (en) * 1990-06-11 1992-08-04 Ford Motor Company Vehicle inertia and center of gravity estimator
DE4423938B4 (de) * 1994-07-07 2007-08-30 Airbus Deutschland Gmbh Anordnung zur elektronischen Messung der Belastung eines Fahrwerks
US5521827A (en) * 1994-09-16 1996-05-28 General Electrodynamics Corporation On-board aircraft weighting and center of gravity determing apparatus and method
US6032090A (en) * 1997-05-06 2000-02-29 General Electrodynamics Corporation System and method for on-board determination of aircraft weight and load-related characteristics
US6913228B2 (en) * 2003-09-04 2005-07-05 Supersonic Aerospace International, Llc Aircraft with active center of gravity control
US7954766B2 (en) * 2005-06-24 2011-06-07 Sikorsky Aircraft Corporation System and method for improved rotary-wing aircraft performance with interior/external loads
US8260477B2 (en) * 2007-12-04 2012-09-04 King Fahd University Of Petroleum And Minerals Method and apparatus for tracking center of gravity of air vehicle
US20110117903A1 (en) * 2009-11-19 2011-05-19 James Roy Bradley Device and method for disabling mobile devices
CN102419238B (zh) * 2011-08-15 2013-12-18 中国航空工业集团公司西安飞机设计研究所 颤振模型质量惯性矩的测量装置
US9361486B2 (en) 2013-11-25 2016-06-07 AeroData, Inc. Determining a profile for an aircraft prior to flight using a fuel vector and uncertainty bands
WO2019061000A1 (en) 2017-09-29 2019-04-04 Bombardier Inc. METHOD, SYSTEM AND GRAPHIC INDICATOR FOR PROVIDING A CENTER OF LATERAL GRAVITY OF AN AIRCRAFT
CN111664994B (zh) * 2020-07-08 2022-07-05 福州大学 一种固定翼飞行器三维转动量测试装置及测试方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2540807A (en) * 1944-05-25 1951-02-06 Gen Electric Center of gravity indicator
US2453607A (en) * 1944-06-06 1948-11-09 Curtiss Wright Corp Center of gravity location indicator
US2541429A (en) * 1949-03-26 1951-02-13 Northrop Aircraft Inc Aircraft balance indicator
US2735291A (en) * 1952-09-27 1956-02-21 Weight and center of gravity computing
US3701279A (en) * 1971-02-08 1972-10-31 Electro Dev Corp Aircraft weight and center of gravity indicator system
US3948096A (en) * 1971-03-16 1976-04-06 Sperry Rand Corporation Apparatus for computing the acceleration of an aircraft along its flight path
US3727180A (en) * 1971-03-23 1973-04-10 Blh Electronics On-board aircraft weight and c. g. synchro-type self-checking attitude sensor
US4032083A (en) * 1976-04-12 1977-06-28 United Technologies Corporation Automatic gain control for stability augmentation systems
US4110605A (en) * 1977-02-25 1978-08-29 Sperry Rand Corporation Weight and balance computer apparatus for aircraft
US4312042A (en) * 1979-12-12 1982-01-19 Sundstrand Data Control, Inc. Weight, balance, and tire pressure detection systems
JPS56108399A (en) * 1980-01-31 1981-08-27 Nippon Electric Co Controller for location of centroid of artificial satellite
US4313201A (en) * 1980-03-05 1982-01-26 United Technologies Corporation Tested, dissimilar helicopter stability augmentation

Also Published As

Publication number Publication date
IT8348538A0 (it) 1983-06-20
AU544746B2 (en) 1985-06-13
GB2122355B (en) 1986-07-16
SE8303431D0 (sv) 1983-06-15
NL8302177A (nl) 1984-01-16
GB8316417D0 (en) 1983-07-20
GB2122355A (en) 1984-01-11
IL68915A (en) 1988-12-30
AU1536183A (en) 1983-12-22
JPS5910827A (ja) 1984-01-20
US4545019A (en) 1985-10-01
NZ204481A (en) 1986-11-12
FR2528978A1 (fr) 1983-12-23
FR2528978B1 (fr) 1986-05-09
CA1211567A (en) 1986-09-16
IT1201068B (it) 1989-01-27
DE3321922A1 (de) 1984-02-09

Similar Documents

Publication Publication Date Title
SE8303431D0 (sv) Metsystem for flygplan
FR2613688B1 (fr) Pylone pour avion
DE3382509D1 (de) Verfahren und vorrichtung zur reduktion der fluegelschwingungen eines flugzeuges mit hilfe aktiver klappen.
NO149421C (no) Anordning for bestemmelse av fluktretningen for et fly
SE8304281D0 (sv) Starrflugel-flugkorper
NL7713354A (nl) Landingsgestel voor een vliegtuig.
SE8404321L (sv) Apparat for att meta troghetsspecifik kraft och vinkelhastighet hos en rorlig kropp och accelerometeraggregat som er speciellt lempligt dertill
DE2967316D1 (en) Method for aiding piloting and landing of an aircraft
FEGLEY Inertial navigation task(Flight tests of strapdown inertial navigation system in helicopter to determine feasibility for simulating systems using inertial navigation equipment)[Final Technical Report]
JPS54131300A (en) Aerodynamic moment generating rudder of aircraft
Ferrier et al. Helicopter/ship analytic dynamic interface
COLLIN et al. Air navigation in the 1980 s- Proposal of an integrated system
Casto Digital emulation of the AH-64 A contrast tracker
Vontein Reasons for increasing development cost of rotary wing aircraft and ideas to reverse the trend
BURTON Fine attitude measurement system study. Volume 1: Executive summary(Final Report)
Toolan et al. Development and simulation testing of an integrated sensory subsystem(ISS) for advanced aircraft(Phase III)
SE8402470L (sv) Varningssystem for alltfor snabb sjunkning for ett taktiskt flygplan
BEZVESILNAIA Laser accelerometers in aerial gravimetry systems
BLINOV et al. New flight simulators at Vnukovo permit less in-flight training
Berube RNAV benefits today- Today and future requirements
HOROWITZ Measurement and effects of transport delays in a state-of-the-art F-16 C flight simulator(Final Report, Aug. 1985- Sep. 1987)
TSUKAMOTO et al. Simulation Analysis of ALFLEX Constrained Flight
FR2371006A1 (en) Approach path control for auto-gyro landing - has velocity and altitude path control to minimise noise and energy consumption during landing
KOCIAN Study of the effects of vibration on inertial navigation system accuracy(M. S. Thesis)
MEYER et al. NASA Ames Active Control Aircraft flight experiments(ACA) program(for short haul aircraft)

Legal Events

Date Code Title Description
NAV Patent application has lapsed

Ref document number: 8303431-4

Format of ref document f/p: F