NDLI: Survivable Engine Control Algorithm Development (SECAD)

Content Provider	IEEE Xplore Digital Library
Author	Frankenberger III, C.E.
Copyright Year	2002
Description	Author affiliation: Weapons Div., Naval Air Warfare Center, China Lake, CA, USA (Frankenberger, C.E., III)
Abstract	This presentation describes the work conducted as part of the Survivable Engine Control Algorithm Development (SECAD) project. The SECAD project was sponsored by the Joint Technical Coordinating Group on Aircraft Survivability (JTCG/AS) Vulnerability Reduction Subgroup and conducted by the Naval Air Warfare Center Weapons Division and General Electric Aircraft Engines, Lynn MA. The overall objective of the SECAD project is to develop turbine engine control algorithms that have the potential to reduce aircraft engine vulnerability to combat damage, including foreign object damage (FOD). The initial development effort was laid out in three-phases. Phase 1 conducted in early FY99, defined candidate engine damage modes to be addressed, and approaches to mitigate the damage effects. In phase 2 damage models, detection algorithms, and mitigation strategies were developed and evaluated using F414 computer engine models. Phase 3 integrated the damage detection algorithms with the F414 control system and an engine test was conducted to demonstrate the capabilities of the concepts developed. During these tests, SECAD successfully detected fan and compressor damage, combustor airflow loss and variable exhaust nozzle loss of control. This presentation documents the successful development and test of the damage detection and mitigation algorithms, and discusses the potential for merging these techniques with current prognostics and health monitoring technologies.
Sponsorship	IEEE Aerosp. & Electron. Syst. Soc
Starting Page	6
Ending Page	6
File Size	482791
Page Count	1
File Format	PDF
ISBN	078037231X
DOI	10.1109/AERO.2002.1036143
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2002-03-09
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Engines Aircraft propulsion Detection algorithms Aerospace control Weapons Turbines Control systems System testing Merging Monitoring
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

The SECAD project - vulnerability reduction via propulsion control logic

Comprehensive engine diagnostic system-CEDS

Reliability analysis of a single-engine aircraft FADEC

Turbine Engine Reconfigurable Control Systems for Aircraft Propulsion Performance Improvement

Recent topics of aircraft engine control systems R&D at TRDI, JDA

On evolutionary optimisation of Markov models of aero engines

F/A-18E/F F414 advanced inflight engine condition monitoring system (IECMS)

C-17 engine-out compensation system testing

A Real-Time Fortran Implementation of a Sensor Failure Detection, Isolation and Accommodation Algorithm

Survivable Engine Control Algorithm Development (SECAD)

Similar Documents

The SECAD project - vulnerability reduction via propulsion control logic

Comprehensive engine diagnostic system-CEDS

Reliability analysis of a single-engine aircraft FADEC

Turbine Engine Reconfigurable Control Systems for Aircraft Propulsion Performance Improvement

Recent topics of aircraft engine control systems R&D at TRDI, JDA

On evolutionary optimisation of Markov models of aero engines

F/A-18E/F F414 advanced inflight engine condition monitoring system (IECMS)

C-17 engine-out compensation system testing

A Real-Time Fortran Implementation of a Sensor Failure Detection, Isolation and Accommodation Algorithm

Survivable Engine Control Algorithm Development (SECAD)