منابع مشابه
Adaptive Quaternion Attitude Control of Aerodynamic Flight Control Vehicles
Conventional quaternion based methods have been extensively employed for spacecraft attitude control where the aerodynamic forces can be neglected. In the presence of aerodynamic forces, the flight attitude control is more complicated due to aerodynamic moments and inertia uncertainties. In this paper, a robust nero-adaptive quat...
متن کاملSHEFEX – Hypersonic Re-entry Flight Experiment Vehicle and Subsystem Design, Flight Performance and Prospects
The purpose of the Sharp Edge Flight Experiment (SHEFEX) was to investigate the aerodynamic behavior and thermal problems of an unconventional shape for re-entry vehicles comprising multi-facetted surfaces with sharp edges. The main object of this experiment was the correlation of numerical analysis with real flight data with respect to the aerodynamic effects and structural concept for the the...
متن کاملBioinspired flight control.
David Lentink Department of Mechanical Engineering, Stanford University, USA E-mail: [email protected] The invention and deployment of small flying robots (drones) is beginning to influence our everyday lives. Their applications are frightening to some and exciting to others. From military surveillance, to city courier services, to near-future flying camera phones, this technology is bound ...
متن کاملToward intelligent flight control
Flight control systems can benefit by being designed to emulate functions of natural intelligence. Intelligent control functions fall in three categories. Declarative actions involve decision making, providing models for system monitoring , goal planning, and systemlscenario identification. Procedural actions concern skilled behavior and have parallels in guidance, navigation, and adaptation. R...
متن کاملReconfigurable flight control system
The article explains the possibility of applying the system of parametric methods, structural reconfiguration control and reconfiguration of the object control objectives to prevent the transition to the current flight situation into a catastrophic one and maintain the specified level of safety. The article presents a block diagram of a control system developed reconfigurable dynamic system, an...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: The Eagle Feather
سال: 2010
ISSN: 2332-4066
DOI: 10.12794/tef.2010.249