Nonlinear life-extending control of a rocket engine

Carl F. Lorenzo; Michael S. Holmes; Asok Ray

doi:10.2514/2.4599

Nonlinear life-extending control of a rocket engine

Carl F. Lorenzo
, Michael S. Holmes
, Asok Ray

Mechanical Engineering

Research output: Contribution to journal › Article › peer-review

6 Scopus citations

Abstract

The conceptual development of a life-extending control (LEC) system is discussed. The LEC is designed for a reusable rocket engine via damage mitigation in both the fuel and oxidizer turbines while achieving high performance for transient responses of the main thrust chamber pressure and the O₂/H₂ mixture ratio.

Original language	English (US)
Pages (from-to)	759-762
Number of pages	4
Journal	Journal of Guidance, Control, and Dynamics
Volume	23
Issue number	4
DOIs	https://doi.org/10.2514/2.4599
State	Published - 2000

All Science Journal Classification (ASJC) codes

Control and Systems Engineering
Aerospace Engineering
Space and Planetary Science
Electrical and Electronic Engineering
Applied Mathematics

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10.2514/2.4599

Cite this

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title = "Nonlinear life-extending control of a rocket engine",

abstract = "The conceptual development of a life-extending control (LEC) system is discussed. The LEC is designed for a reusable rocket engine via damage mitigation in both the fuel and oxidizer turbines while achieving high performance for transient responses of the main thrust chamber pressure and the O2/H2 mixture ratio.",

author = "Lorenzo, \{Carl F.\} and Holmes, \{Michael S.\} and Asok Ray",

year = "2000",

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language = "English (US)",

volume = "23",

pages = "759--762",

journal = "Journal of Guidance, Control, and Dynamics",

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publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

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T1 - Nonlinear life-extending control of a rocket engine

AU - Lorenzo, Carl F.

AU - Holmes, Michael S.

AU - Ray, Asok

PY - 2000

Y1 - 2000

N2 - The conceptual development of a life-extending control (LEC) system is discussed. The LEC is designed for a reusable rocket engine via damage mitigation in both the fuel and oxidizer turbines while achieving high performance for transient responses of the main thrust chamber pressure and the O2/H2 mixture ratio.

AB - The conceptual development of a life-extending control (LEC) system is discussed. The LEC is designed for a reusable rocket engine via damage mitigation in both the fuel and oxidizer turbines while achieving high performance for transient responses of the main thrust chamber pressure and the O2/H2 mixture ratio.

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UR - https://www.scopus.com/pages/publications/0034228295#tab=citedBy

U2 - 10.2514/2.4599

DO - 10.2514/2.4599

M3 - Article

AN - SCOPUS:0034228295

SN - 0731-5090

VL - 23

SP - 759

EP - 762

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

IS - 4

ER -

Nonlinear life-extending control of a rocket engine

Abstract

All Science Journal Classification (ASJC) codes

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