GB854905A - Flight aid systems for aircraft - Google Patents

Flight aid systems for aircraft

Info

Publication number
GB854905A
GB854905A GB19738/60A GB1973860A GB854905A GB 854905 A GB854905 A GB 854905A GB 19738/60 A GB19738/60 A GB 19738/60A GB 1973860 A GB1973860 A GB 1973860A GB 854905 A GB854905 A GB 854905A
Authority
GB
United Kingdom
Prior art keywords
aid systems
aircraft
jan
flight aid
error signal
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
Application number
GB19738/60A
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.)
Sperry Corp
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 GB854905A publication Critical patent/GB854905A/en
Expired 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, 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
    • 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
    • G05D1/04—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

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)
  • Feedback Control In General (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)

Abstract

854,905. Aircraft flight aid systems. SPERRY RAND CORPORATION. Jan. 1, 1957 [Jan. 3, 1956], No. 19738/60. Divided out of 854,904. Drawings to Specification. Class 40 (1). [Also in Group XXXIII] The description is the same as that of Specification 854,904 but the claims are for a system comprising means for supplying an error signal corresponding to the difference between actual and desired airspeed, and means for deriving an output signal proportional to the algebraic sum of this error signal and a further signal representing the pitch attitude of the craft. The system is particularly suitable for enabling the pilot of a helicopter to approach and maintain a desired airspeed. Specifications 854,906 and 854,907 also are referred to.
GB19738/60A 1956-01-03 1957-01-01 Flight aid systems for aircraft Expired GB854905A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US854905XA 1956-01-03 1956-01-03

Publications (1)

Publication Number Publication Date
GB854905A true GB854905A (en) 1960-11-23

Family

ID=22191946

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19738/60A Expired GB854905A (en) 1956-01-03 1957-01-01 Flight aid systems for aircraft

Country Status (1)

Country Link
GB (1) GB854905A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2202199A (en) * 1987-03-21 1988-09-21 Ferranti Plc Helicopter flight director arrangement
GB2314542A (en) * 1996-06-25 1998-01-07 Trevor Henry Pilot flight safety advisor and flight/mission controller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2202199A (en) * 1987-03-21 1988-09-21 Ferranti Plc Helicopter flight director arrangement
GB2202199B (en) * 1987-03-21 1990-08-22 Ferranti Plc Helicopter flight director arrangement
GB2314542A (en) * 1996-06-25 1998-01-07 Trevor Henry Pilot flight safety advisor and flight/mission controller

Similar Documents

Publication Publication Date Title
GB942392A (en) Aircraft flight control systems
GB1218112A (en) Failure monitor for aricraft automatic pilots
GB854905A (en) Flight aid systems for aircraft
GB854906A (en) Flight aid systems for rotary wing aircraft
GB1057562A (en) Improvements in or relating to air data computers
GB854907A (en) Flight aid systems for aircraft
GB829740A (en) Aircraft pitch-attitude control apparatus
GB951444A (en) Integrated flight instrument system
GB854734A (en) Aircraft guidance apparatus
GB803576A (en) Control systems for aircraft
GB877789A (en) Aircraft flight control systems
CA597468A (en) Control systems for aircraft engines
GB854733A (en) Aircraft control systems
CA525954A (en) Systems for controlling the attitude of aircraft in flight, and other control systems, responsive to a rate of change of a condition
GB877172A (en) Improvements in or relating to automatic blind landing systems for aircraft
AU220917B2 (en) Flight control systems for aircraft
AU219078B2 (en) Aircr aft flying control systems
WUEST et al. Design problems of the Airbus A 300 B forward thrust regulator(Specification of thrust control system for Airbus A 300 B, tested in Boeing 707)
GB863457A (en) Vertical reference-defining apparatus
GB1028676A (en) Improvements in and relating to the aligning of twin-component aviation systems in flight
CA564988A (en) Pitch control servo system for an aeronautical propeller
AU2176656A (en) Aircr aft flying control systems
GB866015A (en) Aircraft flight instruments
MOREINES The application of redundancy to achieve a fail-operative flight control system(Triple redundant flight control system for fail operative performance)
GB1219289A (en) Improvements in and relating to aircraft landing systems