Proceedings of the 2004 IEEE International Conference on Control Applications, 2004.
DOI: 10.1109/cca.2004.1387216
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Estimation of thrust and mass flow in a jet engine

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Cited by 2 publications
(3 citation statements)
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“…Since a LTI engine model is used as the plant whose outputs readily includes thrust, thrust estimation techniques such as those proposed in references in [63,64,65] can be avoided since the estimated thrust is almost identical to the actual thrust produced. MPC being a model based technique uses a reference model whose output includes the thrust produced, which can be weighted accordingly.…”
Section: Thrust Control Simulationsmentioning
confidence: 99%
“…Since a LTI engine model is used as the plant whose outputs readily includes thrust, thrust estimation techniques such as those proposed in references in [63,64,65] can be avoided since the estimated thrust is almost identical to the actual thrust produced. MPC being a model based technique uses a reference model whose output includes the thrust produced, which can be weighted accordingly.…”
Section: Thrust Control Simulationsmentioning
confidence: 99%
“…The jet engine model is composed of two parts. The first one refers to a system of static nonlinear equations that describe the thermodynamic relations in the compressor, turbine and nozzle as follows: 13,14…”
Section: Hardware-in-the-loop Frameworkmentioning
confidence: 99%
“…The compressor duct along with the combustion chamber are assumed to control volume. The transient equations for the combustion chamber volume are as follows 14,15…”
Section: Hardware-in-the-loop Frameworkmentioning
confidence: 99%