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System Identification of an Octocopter in Hover using Full-Harmonic Orthogonal Multisine Inputs
A new method for multi-input flight maneuver design for system identification is presented. The method consists of injecting "full-harmonic" orthogonal multisine signals into the flight control system. Orthogonality is achieved by repeating maneuvers with changing multisine polarities. The multisine
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