Improvements in the transient fidelity of HWIL flight tables using acceleration feedback

Details Improvements in the transient fidelity of HWIL flight tables using acceleration feedback Improvements in the transient fidelity of HWIL flight tables using acceleration feedback

Jul 2002

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002spie.4717...32s&link_type=abstract

Proc. SPIE Vol. 4717, p. 32-45, Technologies for Synthetic Environments: Hardware-in-the-Loop Testing VII, Robert Lee Murrer; Ed

Physics

Scientific paper

Control system architecture will help eliminate or reduce non-linear behavior of flight table axes motions. This elimination and reduction will help improve dynamic transparency in HWIL simulations. This paper presents the design, analysis and test results of a three-axis hydraulic flight table using acceleration feedback as a part of the axes servo structure. This approach significantly improves the transient motion of the axis under control producing a very high fidelity flight motion table.

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