@inproceedings{95e4a60bb2454c9a95b44041f2c2ec0c,
title = "Linear state variable dynamic model and estimator design for Allison 1406 gas turbine engine",
abstract = "This paper describes a procedure for developing a State Variable Model for the Allison T406 gas turbine engine. This linear model is useful for designing controllers using modern control techniques. The engine and V-22 rotor system is modeled around an operating point by using four state variables and one input variable. For a given power setting, it is observed that two linear models are sufficient to represent the engine dynamics over the entire flight envelope. A relationship between surge margin and the state variables is also developed. It is demonstrated that these linear models are useful in designing an estimator for accommodating hard sensor failures.",
author = "{Vittal Rao}, S. and D. Moellenhoff and Jaeger, {J. A.}",
note = "Publisher Copyright: Copyright {\textcopyright} 1988 by ASME.; null ; Conference date: 06-06-1988 Through 09-06-1988",
year = "1988",
doi = "10.1115/88-GT-239",
language = "English",
series = "Proceedings of the ASME Turbo Expo",
publisher = "American Society of Mechanical Engineers (ASME)",
booktitle = "Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation",
}