TW200504480A - Flight control system with adaptive control and malfunction detection - Google Patents

Flight control system with adaptive control and malfunction detection

Info

Publication number
TW200504480A
TW200504480A TW092120311A TW92120311A TW200504480A TW 200504480 A TW200504480 A TW 200504480A TW 092120311 A TW092120311 A TW 092120311A TW 92120311 A TW92120311 A TW 92120311A TW 200504480 A TW200504480 A TW 200504480A
Authority
TW
Taiwan
Prior art keywords
control
aircraft
flight
malfunction detection
control system
Prior art date
Application number
TW092120311A
Other languages
Chinese (zh)
Other versions
TWI242700B (en
Inventor
Chun-Liang Lin
Kung-Shing Huang
Jun-De Liu
bo-guang Zhang
Wen-Jie Kang
Original Assignee
Ind Tech Res Inst
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 Ind Tech Res Inst filed Critical Ind Tech Res Inst
Priority to TW92120311A priority Critical patent/TWI242700B/en
Publication of TW200504480A publication Critical patent/TW200504480A/en
Application granted granted Critical
Publication of TWI242700B publication Critical patent/TWI242700B/en

Links

Landscapes

  • Selective Calling Equipment (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

The present invention provides a flight control system with adaptive control and malfunction detection. The pilot of the aircraft can enter commands from the cockpit and control the aircraft via a controller. Then a sensor is employed to measure the actual data to compare with the ideal data for total error estimation. A control interface abnormal recognizing means is employed to determine whether a certain hardware is malfunction, and further perform an internal parameter modification to feed back to the controller by a parameter updating rule and neural fuzzy network, so as to change the control of related hardware for the aircraft to rapidly stabilize the aircraft thereby assuring the flight security.
TW92120311A 2003-07-25 2003-07-25 Flight control system with adaptive control and malfunction detection TWI242700B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW92120311A TWI242700B (en) 2003-07-25 2003-07-25 Flight control system with adaptive control and malfunction detection

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW92120311A TWI242700B (en) 2003-07-25 2003-07-25 Flight control system with adaptive control and malfunction detection

Publications (2)

Publication Number Publication Date
TW200504480A true TW200504480A (en) 2005-02-01
TWI242700B TWI242700B (en) 2005-11-01

Family

ID=37022572

Family Applications (1)

Application Number Title Priority Date Filing Date
TW92120311A TWI242700B (en) 2003-07-25 2003-07-25 Flight control system with adaptive control and malfunction detection

Country Status (1)

Country Link
TW (1) TWI242700B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104507799A (en) * 2014-04-28 2015-04-08 深圳市大疆创新科技有限公司 Protection control method of air vehicle, device and air vehicle
US9789969B2 (en) 2014-02-27 2017-10-17 SZ DJI Technology Co., Ltd. Impact protection apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9789969B2 (en) 2014-02-27 2017-10-17 SZ DJI Technology Co., Ltd. Impact protection apparatus
CN104507799A (en) * 2014-04-28 2015-04-08 深圳市大疆创新科技有限公司 Protection control method of air vehicle, device and air vehicle

Also Published As

Publication number Publication date
TWI242700B (en) 2005-11-01

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Legal Events

Date Code Title Description
MM4A Annulment or lapse of patent due to non-payment of fees