http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-8473124-B2

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publicationDate 2013-06-25-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-8473124-B2
titleOfInvention Flight control system having a three control loop design
abstract A flight control system is configured for controlling the flight of an aircraft utilizing a three control loop design to robustly increase system performance. An inner loop comprises an improved linear quadratic regulator (LQR) search method, and an outer loop comprises a classic feedback summary gain design. A third loop comprises a steady state trim search method.
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Total number of triples: 53.