GB2136605B - Helicopter attitude and airspeed acquisition and retention system - Google Patents

Helicopter attitude and airspeed acquisition and retention system

Info

Publication number
GB2136605B
GB2136605B GB08401178A GB8401178A GB2136605B GB 2136605 B GB2136605 B GB 2136605B GB 08401178 A GB08401178 A GB 08401178A GB 8401178 A GB8401178 A GB 8401178A GB 2136605 B GB2136605 B GB 2136605B
Authority
GB
United Kingdom
Prior art keywords
airspeed
acquisition
autopilot
retention system
engaged
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
GB08401178A
Other versions
GB8401178D0 (en
GB2136605A (en
Inventor
Douglas Harold Clelford
Richard Dennis Murphy
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.)
Raytheon Technologies Corp
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
Priority claimed from US06/176,832 external-priority patent/US4382283A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of GB8401178D0 publication Critical patent/GB8401178D0/en
Publication of GB2136605A publication Critical patent/GB2136605A/en
Application granted granted Critical
Publication of GB2136605B publication Critical patent/GB2136605B/en
Expired legal-status Critical Current

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
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • 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
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Navigation (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Mechanical Control Devices (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

The description is substantially identical to that of Patent Specification GB 2081474A but the claims are directed to a helicopter pitch axis autopilot system with provision for manual override when the cyclic pitch control stick is moved away from its trim position, the system memorising the trim position so that the autopilot can subsequently be re-engaged. When the autopilot is re-engaged an airspeed error limiter ensures a smooth transition.
GB08401178A 1980-08-08 1984-01-17 Helicopter attitude and airspeed acquisition and retention system Expired GB2136605B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/176,832 US4382283A (en) 1980-08-08 1980-08-08 Helicopter attitude and airspeed acquisition and retention system
GB8121053A GB2081474B (en) 1980-08-08 1981-07-08 Helicopter attitude and airspeed acquisition and retention system

Publications (3)

Publication Number Publication Date
GB8401178D0 GB8401178D0 (en) 1984-02-22
GB2136605A GB2136605A (en) 1984-09-19
GB2136605B true GB2136605B (en) 1985-05-15

Family

ID=26280057

Family Applications (4)

Application Number Title Priority Date Filing Date
GB08401178A Expired GB2136605B (en) 1980-08-08 1984-01-17 Helicopter attitude and airspeed acquisition and retention system
GB08401176A Expired GB2136603B (en) 1980-08-08 1984-01-17 Helicopter attitude and airspeed acquisition and retention system
GB08401177A Expired GB2136604B (en) 1980-08-08 1984-01-17 Helicopter attitude and airspeed acquisition and retention system
GB08401179A Expired GB2136576B (en) 1980-08-08 1984-01-17 Helicopter airspeed measuring system

Family Applications After (3)

Application Number Title Priority Date Filing Date
GB08401176A Expired GB2136603B (en) 1980-08-08 1984-01-17 Helicopter attitude and airspeed acquisition and retention system
GB08401177A Expired GB2136604B (en) 1980-08-08 1984-01-17 Helicopter attitude and airspeed acquisition and retention system
GB08401179A Expired GB2136576B (en) 1980-08-08 1984-01-17 Helicopter airspeed measuring system

Country Status (1)

Country Link
GB (4) GB2136605B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2610411B1 (en) * 1987-02-04 1989-06-09 Sfim METHOD AND DEVICE FOR MEASURING THE SPEED IN RELATION TO THE AIR OF A LOW-SPEED HELICOPTER
FR2741855B1 (en) * 1995-12-05 1998-01-30 Eurocopter France CYCLIC SLEEVE SYSTEM FOR SPEED STABILITY OF A HELICOPTER
US10747235B2 (en) 2018-04-25 2020-08-18 The Boeing Company Pitch trim prediction for aircraft
EP3561631B1 (en) * 2018-04-25 2022-11-23 The Boeing Company Pitch and thrust control for compound aircraft
US11312480B2 (en) 2018-06-01 2022-04-26 Textron Innovations Inc. System and method for controlling rotorcraft
EP3677505B1 (en) * 2019-01-02 2024-03-20 Textron Innovations Inc. System and method for controlling rotorcraft

Also Published As

Publication number Publication date
GB8401176D0 (en) 1984-02-22
GB8401177D0 (en) 1984-02-22
GB2136576B (en) 1985-03-27
GB2136603A (en) 1984-09-19
GB2136603B (en) 1985-06-05
GB8401179D0 (en) 1984-02-22
GB2136576A (en) 1984-09-19
GB8401178D0 (en) 1984-02-22
GB2136604B (en) 1985-03-27
GB2136604A (en) 1984-09-19
GB2136605A (en) 1984-09-19

Similar Documents

Publication Publication Date Title
ES8203757A1 (en) Helicopter attitude and airspeed acquisition and retention system
SE8400997D0 (en) AUTOMATIC LIMITATION OF THE TORQUE OF A HELICOPTER ENGINE
GB2136605B (en) Helicopter attitude and airspeed acquisition and retention system
US4312039A (en) Transient free synchronization system
IL59194A (en) Helicopter control means for desensitizing inadvertent pilot commands
GB1023831A (en) Automatic trim correcting system for aircraft
US3805033A (en) Autopilot go-around mode pitch command signal computations
US3361394A (en) Flight control system
GB1013869A (en) Automatic pilot effecting controlled speed followed by asymptotic approach to selected altitude
US3105660A (en) Automatic flight control system
FR2334942A1 (en) Control of approach of aircraft during landing - regulates deceleration in accordance with total slope compared with reference slope
GB1182541A (en) Automatic Pilots for Aircraft
GB926559A (en) Control system for helicopter
FR2371006A1 (en) Approach path control for auto-gyro landing - has velocity and altitude path control to minimise noise and energy consumption during landing
Gibson Flying qualities and the fly-by-wire aeroplane
GB941006A (en) Aircraft automatic control systems
NADKARNI et al. Comparative study of flare control laws(optimal control of b-737 aircraft approach and landing)[Progress Report, 15 Dec. 1977- 14 Dec. 1978]
HORWITZ Development of a gyro-less digital flight director(Digital flight director for precise aircraft control)
CA589931A (en) Helicopter with automatic pitch control
EP0372660A3 (en) Flight path angle command, flight control system for landing flare
KELLEY et al. Variable-sweep optimization(for hodograph-vector-control concept in maneuvering flight)
FR2406244A2 (en) Approach path control for auto-gyro landing - has velocity and altitude path control to minimise noise and energy consumption during landing
JPS5313270A (en) Apparatus for feeding materials
TRANKLE Autopilot logic for the flare maneuver of STOL aircraft[Ph. D. Thesis]
Frey et al. Design and simulation of automatic aircraft landing systems

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19980708