CA1317008C - Systeme de guidage d'aeronef en approche de precision - Google Patents

Systeme de guidage d'aeronef en approche de precision

Info

Publication number
CA1317008C
CA1317008C CA000574131A CA574131A CA1317008C CA 1317008 C CA1317008 C CA 1317008C CA 000574131 A CA000574131 A CA 000574131A CA 574131 A CA574131 A CA 574131A CA 1317008 C CA1317008 C CA 1317008C
Authority
CA
Canada
Prior art keywords
aircraft
landing
control
during
precision approach
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
CA000574131A
Other languages
English (en)
Inventor
Romeo P. Martorella
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.)
Grumman Corp
Original Assignee
Grumman Aerospace 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 Grumman Aerospace Corp filed Critical Grumman Aerospace Corp
Application granted granted Critical
Publication of CA1317008C publication Critical patent/CA1317008C/fr
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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G05D1/0684—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing on a moving platform, e.g. aircraft carrier

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
CA000574131A 1987-08-13 1988-08-08 Systeme de guidage d'aeronef en approche de precision Expired - Fee Related CA1317008C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US8546187A 1987-08-13 1987-08-13
US085,461 1987-08-13

Publications (1)

Publication Number Publication Date
CA1317008C true CA1317008C (fr) 1993-04-27

Family

ID=22191768

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000574131A Expired - Fee Related CA1317008C (fr) 1987-08-13 1988-08-08 Systeme de guidage d'aeronef en approche de precision

Country Status (6)

Country Link
JP (1) JPH01119500A (fr)
CA (1) CA1317008C (fr)
DE (1) DE3827482A1 (fr)
FR (1) FR2619458A1 (fr)
GB (1) GB2208631B (fr)
IL (1) IL87382A (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3621052A1 (de) * 1986-06-24 1988-01-07 Aerodata Flugmesstechnik Gmbh Vorrichtung zur automatischen flugbahnfuehrung von flugzeugen laengs eines leitstrahls
DE4300761A1 (de) * 1993-01-14 1994-07-21 Erno Raumfahrttechnik Gmbh Vorrichtung zur Steuerung
US7609204B2 (en) 2005-08-30 2009-10-27 Honeywell International Inc. System and method for dynamically estimating output variances for carrier-smoothing filters
FR2909462B1 (fr) * 2006-12-05 2008-12-26 Airbus France Sas Procede et dispositif de controle actif du tangage d'un avion.
EP2151730A1 (fr) * 2008-08-05 2010-02-10 The Boeing Company Navigation d'un avion en quatre dimensions
CN104536462A (zh) * 2015-01-09 2015-04-22 西安应用光学研究所 基于光纤陀螺积分手段的位置控制方法
CN117452974B (zh) * 2023-12-22 2024-04-09 中国航空工业集团公司西安飞机设计研究所 一种运输机机场短距着陆优化方法及装置

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3586268A (en) * 1969-04-04 1971-06-22 William W Melvin Instrument flight system
US3626163A (en) * 1970-01-28 1971-12-07 Us Army Automatic landing system
US3743221A (en) * 1970-04-09 1973-07-03 Lear Siegler Inc Aircraft flight control apparatus
US3714825A (en) * 1970-12-29 1973-02-06 W Melvin Instrument flight system
US4040005A (en) * 1974-12-23 1977-08-02 Melvin William W Composite situation analyzer and instrument flight system
FR2559123B1 (fr) * 1984-02-03 1988-11-10 Hirsch Rene Procede et dispositif pour compenser les rafales subies par un avion en vol
US4709336A (en) * 1985-01-09 1987-11-24 Sperry Corporation Descent flight path control for aircraft

Also Published As

Publication number Publication date
DE3827482A1 (de) 1989-04-06
IL87382A (en) 1994-07-31
GB2208631B (en) 1991-06-26
GB2208631A (en) 1989-04-12
FR2619458A1 (fr) 1989-02-17
GB8819093D0 (en) 1988-09-14
JPH01119500A (ja) 1989-05-11

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Legal Events

Date Code Title Description
MKLA Lapsed
MKLA Lapsed

Effective date: 19970428