An aerial vehicle comprising an airframe, an aircraft flight controller to provide an output control signal, and a planar printed circuit board positioned on the airframe. The printed circuit board may include coupled thereto a processor, a rate gyroscope, and at least three accelerometers. The processor is configured to generate an actuation signal based at least in part on a feedback signal received from at least one of said rate gyroscope and the at least three accelerometers. The processor communicates the actuation signal to said aircraft flight controller, which is configured to adjust the output control signal based on said actuation signal.
DISTRIBUTED ACCELERATION SENSING FOR ROBUST DISTURBANCE REJECTION
VERTEILTE BESCHLEUNIGUNGSERFASSUNG FÜR ROBUSTE STÖRUNTERDRÜCKUNG
DÉTECTION D'ACCÉLÉRATION DISTRIBUÉE POUR UN REJET DE PERTURBATION ROBUSTE
2020-06-24
Patent
Electronic Resource
English
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