WO2008097319A3 - Autonomous outer loop control of man-rated fly-by-wire aircraft - Google Patents

Autonomous outer loop control of man-rated fly-by-wire aircraft Download PDF

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Publication number
WO2008097319A3
WO2008097319A3 PCT/US2007/069749 US2007069749W WO2008097319A3 WO 2008097319 A3 WO2008097319 A3 WO 2008097319A3 US 2007069749 W US2007069749 W US 2007069749W WO 2008097319 A3 WO2008097319 A3 WO 2008097319A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
fly
fbw
rated
man
Prior art date
Application number
PCT/US2007/069749
Other languages
French (fr)
Other versions
WO2008097319A2 (en
Inventor
Louis H Knotts
Eric E Ohmit
Original Assignee
Calspan Corp
Louis H Knotts
Eric E Ohmit
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 Calspan Corp, Louis H Knotts, Eric E Ohmit filed Critical Calspan Corp
Publication of WO2008097319A2 publication Critical patent/WO2008097319A2/en
Publication of WO2008097319A3 publication Critical patent/WO2008097319A3/en

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Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft

Abstract

The present invention is directed to a control system for use on a fly-by-wire (FBW) aircraft. The system includes a controller coupled to the FBW aircraft. The controller is configured to generate a plurality of simulated pilot control signals from at least one aircraft maneuver command. The plurality of simulated pilot control signals are generated in accordance with a predetermined control law. The at least one aircraft maneuver command is derived from at least one command telemetry signal received from a remote control system not disposed on the FBW aircraft. The plurality of simulated pilot control signals are configured to direct the FBW aircraft to perform an aircraft maneuver in accordance with the at least one aircraft maneuver command.
PCT/US2007/069749 2006-06-21 2007-05-25 Autonomous outer loop control of man-rated fly-by-wire aircraft WO2008097319A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US24560006A 2006-06-21 2006-06-21
US11/245,600 2006-06-21

Publications (2)

Publication Number Publication Date
WO2008097319A2 WO2008097319A2 (en) 2008-08-14
WO2008097319A3 true WO2008097319A3 (en) 2009-01-15

Family

ID=39682253

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2007/069749 WO2008097319A2 (en) 2006-06-21 2007-05-25 Autonomous outer loop control of man-rated fly-by-wire aircraft

Country Status (1)

Country Link
WO (1) WO2008097319A2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015135194A1 (en) * 2014-03-14 2015-09-17 深圳市大疆创新科技有限公司 Unmanned air vehicle and data processing method therefor
EP3812279B1 (en) 2016-02-29 2022-04-13 SZ DJI Technology Co., Ltd. Method for processing a throttle control signal and electronic speed control
CN107878739B (en) * 2016-09-29 2020-12-22 北京理工大学 Unmanned helicopter control system and control method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4646241A (en) * 1984-06-21 1987-02-24 United Technologies Corporation Solid-state flight data recording system
US4855822A (en) * 1988-01-26 1989-08-08 Honeywell, Inc. Human engineered remote driving system
US5240207A (en) * 1992-08-03 1993-08-31 The United States Of America As Represented By The Secretary Of The Navy Generic drone control system
US6181989B1 (en) * 1999-10-22 2001-01-30 Joseph Andrew Gwozdecki Aircraft attitude sensor and feedback control system
US6742741B1 (en) * 2003-02-24 2004-06-01 The Boeing Company Unmanned air vehicle and method of flying an unmanned air vehicle

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4646241A (en) * 1984-06-21 1987-02-24 United Technologies Corporation Solid-state flight data recording system
US4855822A (en) * 1988-01-26 1989-08-08 Honeywell, Inc. Human engineered remote driving system
US5240207A (en) * 1992-08-03 1993-08-31 The United States Of America As Represented By The Secretary Of The Navy Generic drone control system
US6181989B1 (en) * 1999-10-22 2001-01-30 Joseph Andrew Gwozdecki Aircraft attitude sensor and feedback control system
US6742741B1 (en) * 2003-02-24 2004-06-01 The Boeing Company Unmanned air vehicle and method of flying an unmanned air vehicle

Also Published As

Publication number Publication date
WO2008097319A2 (en) 2008-08-14

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