SCOPUS 정보 검색 플랫폼

Procedia Engineering

Volumn 15, Issue , 2011, Pages 220-224

A method of fault diagnosis and flight envelop assessment for flight control systems

(4) Liu, Xiaoxiong a Chen, Kang a Qiu, Yueheng a Sun, Liyuan a

a NORTHWESTERN POLYTECHNICAL UNIVERSITY (China)

Author keywords

Control surface damage; Fault diagnosis; Flight envelop assessment; The least square method

Indexed keywords

AERODYNAMIC PARAMETERS; CONTROL SURFACE DAMAGE; DAMAGE MODEL; DECISION TECHNOLOGY; FLIGHT ENVELOP; IDENTIFICATION PARAMETERS; LEAST SQUARE METHODS; ON-LINE FAULT DIAGNOSIS; RECURSIVE LEAST SQUARE METHODS;

AERODYNAMICS; AIRCRAFT CONTROL; CONTROL SURFACES; CONTROLLABILITY; DAMAGE DETECTION; FAILURE ANALYSIS; INFORMATION SCIENCE; LEAST SQUARES APPROXIMATIONS; RATING;

FLIGHT CONTROL SYSTEMS;

EID: 84055190622 PISSN: 18777058 EISSN: None Source Type: Conference Proceeding
DOI: 10.1016/j.proeng.2011.08.044 Document Type: Conference Paper

Times cited : (1)

References (6)

1
- 78651089136
- Dynamic flight envelope assessment and prediction
- Urnes, J. M., Reichenbach, Sr. E. Y., and Smith, T. A., Dynamic Flight Envelope Assessment and Prediction, AIAA Guidance Navigation and Control Conference, 2008, p:1-8
- (2008) AIAA Guidance Navigation and Control Conference , pp. 1-8
- Urnes, J.M.¹ Reichenbach Sr., E.Y.² Smith, T.A.³

2
- 77953769920
- An integrated aircraft health assessment and fault contingency management system
- Honolulu, Hawaii
- Tang, L., Roemer, M., Bharadwaj, S., and Belcastro, C., An Integrated Aircraft Health Assessment and Fault Contingency Management System, AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, 2008, p:1-6
- (2008) AIAA Guidance, Navigation and Control Conference and Exhibit , pp. 1-6
- Tang, L.¹ Roemer, M.² Bharadwaj, S.³ Belcastro, C.⁴

3
- 77958188622
- Real-time dynamic modeling - Data information requirements and flight test results
- Eugene A. Morelli, Mark S. Smith, Real-Time Dynamic Modeling - Data Information Requirements and Flight Test Results, AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2008, p:1-28
- (2008) AIAA Atmospheric Flight Mechanics Conference and Exhibit , pp. 1-28
- Morelli, E.A.¹ Smith, M.S.²

4
- 78049260114
- Reachability and region of attraction analysis applied to GTM dynamic flight envelope assessment
- Chicago, Illinois
- Rohit Pandita, Abhijit Chakraborty, Peter Seiler and Gary Balas, Reachability and Region of Attraction Analysis Applied to GTM Dynamic Flight Envelope Assessment, AIAA Guidance, Navigation, and Control, Chicago, Illinois, 2009, p:1-21
- (2009) AIAA Guidance, Navigation, and Control , pp. 1-21
- Pandita, R.¹ Chakraborty, A.² Seiler, P.³ Gar, Y.⁴

5
- 79952732851
- On-line fault diagnosis for control surface of multi-control effector flying wings
- Huang Chengtao, Wang Lixin, On-line fault diagnosis for control surface of multi-control effector flying wings, Acta Aeronautica et astronautica sinica, 2011, 32(1): 58-66
- (2011) Acta Aeronautica et Astronautica Sinica , vol.32 , Issue.1 , pp. 58-66
- Chengtao, H.¹ Wan, G.²

6
- 23444432234
- A better OnLine identification algorithm with impairment of aircraft control surfaces considered
- Su Haoqin, Song Shujie, Deng Jianhua, A Better OnLine Identification Algorithm with Impairment of Aircraft Control Surfaces Considered, Journal of Northwestern Polytechnical University, 2005, 23(3):316-321
- (2005) Journal of Northwestern Polytechnical University , vol.23 , Issue.3 , pp. 316-321
- Su, H.¹ Son, G.² Den, G.³

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.