Srinathkumar, S and Madhuranath, Padma and Girija, G and Niranjana, T and Balakrishna, S (1993) Recent contributions to system theoretic approach to flight mechanics research 13; 13;. In: Proceedings of the International Symposium on Recent Advances in Aerospace Sciences and Engineering, 12-15 Dec 1992, Bangalore, India.Full text not available from this repository.
With the advent of control configured vehicle technology, the design concepts of contemporary high-performance aircraft have undergone revolutionary changes. The extreme reliability of present-day airborne sensors, flight computers, and high-performance actuators has made it possible to design aircraft control systems as full-authority, carefree maneuvering systems using fly-by-wire technology, resulting in the successful development of longitudinally statically unstable airframes. Along with the advances in control technology, the developments in system identification theory have resulted in improved methods of aircraft parameter estimation using flight data. A consequence of all this advancement is the key role flight mechanics and system theory together play in the analysis and optimization of aircraft performance.
|Item Type:||Conference or Workshop Item (Paper)|
|Uncontrolled Keywords:||Flight Mechanics;Aircraft maneuvers;Neural nets;Aircraft control;Longitudinal stability;Aircraft stability;Parameter identification;Wind tunnel models|
|Subjects:||AERONAUTICS > Aircraft Design, Testing & Performance|
|Division/Department:||Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division|
|Depositing User:||Mrs Manoranjitha M D|
|Date Deposited:||05 Mar 2008|
|Last Modified:||24 Aug 2015 14:42|
Actions (login required)