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Damage-mitigating control of space propulsion systems for high performance and extended lifeCalculations are presented showing that a substantial improvement in service life of a reusable rocket engine can be achieved by an insignificant reduction in the system dynamic performance. The paper introduces the concept of damage mitigation and formulates a continuous-time model of fatigue damage dynamics. For control of complex mechanical systems, damage prediction and damage mitigation are carried out based on the available sensory and operational information such that the plant can be inexpensively maintained and safely and efficiently steered under diverse operating conditions. The results of simulation experiments are presented for transient operations of a reusable rocket engine.
Document ID
19930065910
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ray, Asok
(NASA Lewis Research Center Cleveland, OH, United States)
Wu, Min-Kuang
(NASA Lewis Research Center Cleveland, OH, United States)
Dai, Xiaowen
(NASA Lewis Research Center Cleveland, OH, United States)
Carpino, Marc
(Pennsylvania State Univ. University Park, United States)
Lorenzo, Carl F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 93-2080
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: AIAA, ASME, ASEE, SAE
Accession Number
93A49907
Funding Number(s)
CONTRACT_GRANT: NSF ECS-92-16386
CONTRACT_GRANT: NAG3-1240
Distribution Limits
Public
Copyright
Other

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