Dynamic stability testing of the orbiter flight control system/flexible body interaction

1982 ◽  
Author(s):  
R. EPPLE ◽  
R. ALTENBACH
2021 ◽  
Author(s):  
Mária Jabrocká ◽  
◽  
Martin Bugaj

Automation, robotic, unconventional arrangement hydrogen are the hallmarks of new trends in aircraft design. The implementation of hydrogen fuel in aircraft appears to be one of the biggest advances in the near future. Automation in aircraft control is based on the reduction of runway requirements. Among the main conclusions of the paper we include the finding that the aircraft does not have to have a classic conventional arrangement of vertical tail surfaces in order to achieve static/dynamic stability of the aircraft. The complexity of the elements of the aircraft stability and flight control system is directly depended on the weight of the aircraft. Upcoming trends in aircraft design should only based on existing concepts.


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