Output Error Method and Two Step Method for Aerodynamic Model Identification
AIAA Guidance, Navigation, and Control Conference and Exhibit
2005-01-01
Conference paper
Electronic Resource
English
Aerodynamic Parameter Identification of UAV Based on Output-Error Method
Trans Tech Publications | 2014
|Identification of Aerodynamic Derivatives of a Flexible Aircraft Using Output Error Method
Trans Tech Publications | 2011
|Identification of Aerodynamic Derivatives of a Flexible Aircraft Using Output Error Method
British Library Conference Proceedings | 2012
|