Flexible Aerospace Vehicles Simulation and Nonlinear Control Synthesis
| Authors: | Nebylov Alexander, State University of Aerospace Instrumentation, Russian Federation
Brodsky Sergey, State University of Aerospace Instrumentation, Russian Federation
Panferov Alexander, State University of Aerospace Instrumentation, Russian Federation |
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| Topic: | 7.3 Aerospace |
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| Session: | Nonlinear Dynamics and Robust Control in Aerospace Systems |
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| Keywords: | Flight control, flexible vehicle, control system, simulation, bending, sloshing,local angle of attack, control law, robust control, nonlinear systems. |
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Abstract
Possible approaches to the mathematical description of different types of flexible flying vehicles (FFV), and also the principles of universal software construction for control system synthesis, dynamic properties research and FFV motion modeling are observed. The program is stocked with the program modules library. These modules are designed on the base of mathematical models of FFV elements and control system, and also significant physical effects such as flexibility, liquid oscillations, time lag of engines, local aerodynamic effects, etc. Programming modules selection allows to investigate dynamic properties of known and perspective FFV and to develop the effective control systems for their stabilization and motion control.
