Aircraft System Identification

Author: Editorial Committee of Military Training Textbooks, General Armament Department of the Chinese People's Liberation Army
Publisher:
Publish Date: 2003-05-01
Features: This book applies system identification theory to aircraft dynamics systems, explaining how to identify aircraft aerodynamic parameters, aerothermodynamic parameters, engineering turbulence model parameters, and inertial instrument error parameters from various data sources such as remote measurement data from flight experiments, dynamic test data of wind tunnel models, measured flow field parameter data, optical data of free-flight models from ballistic ranges, and temperature data from aircraft model thermal test experiments. This is done to establish a correct mathematical model of the aircraft dynamics system. The book is divided into two parts: theory and application. The theoretical part concisely discusses the basic theories and methods of system identification, while the application part closely combines practical problems in aircraft testing, providing examples, specific algorithms, and formulas. It is a systematic identification textbook that closely integrates theory and practice. The target readers of this book are researchers, engineers, technicians, university teachers, and graduate students engaged in system identification and dynamic characteristics research in the fields of aviation, aerospace, and ordnance, especially those involved in data processing and analysis of flight experiments and wind tunnel experiments. It can also serve as a reference for professionals in system control, system simulation, and system identification research.