CPC F02C 9/00 (2013.01) [B64D 27/02 (2013.01); B64D 27/026 (2024.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2240/60 (2013.01); F05D 2260/80 (2013.01); F05D 2270/09 (2013.01); F05D 2270/20 (2013.01); F05D 2270/44 (2013.01); F05D 2270/80 (2013.01)] | 18 Claims |
1. A hybrid electric propulsion system comprising:
a gas turbine engine comprising at least one compressor section and at least one turbine section operably coupled to a shaft;
an electric motor configured to augment rotational power of the shaft of the gas turbine engine; and
a controller operable to:
determine a plurality of hybrid electric propulsion system parameters based on a composite system model and sensor data from one or more sensors;
determine a prediction based on the hybrid electric propulsion system parameters and the composite system model;
determine a model predictive control optimization for a plurality of hybrid electric system control effectors based on the prediction using a plurality of reduced-order partitions of the composite system model, wherein the reduced-order partitions comprise partitions of a propulsion system model comprising a gas turbine engine model, a mechanical power transmission model, and an electrical power system model;
update a plurality of composite system model states of the composite system model based on detection of one or more faults, wherein the reduced-order partitions of the composite system model comprise a plurality of reduced-order partitions of the composite system model states; and
actuate the hybrid electric system control effectors based on the model predictive control optimization.
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