Data processing: structural design – modeling – simulation – and em – Simulating nonelectrical device or system – Mechanical
Reexamination Certificate
2006-12-05
2006-12-05
Thangavelu, Kandasamy (Department: 2123)
Data processing: structural design, modeling, simulation, and em
Simulating nonelectrical device or system
Mechanical
C434S037000, C244S191000, C244S203000
Reexamination Certificate
active
07146299
ABSTRACT:
The present invention is a system and method for easily adjusting flight characteristics of a simulated aircraft. The system allows a user to adjust commanded pitch, roll or yaw values or steady state frequency response values that are associated with an atmospheric temperature value, an atmospheric dynamic pressure value, aileron position, rudder position, and elevator position.
REFERENCES:
patent: 4840328 (1989-06-01), Sundermeyer
patent: 5437756 (1995-08-01), Carlos et al.
patent: 5607307 (1997-03-01), Shefchunas
patent: 5689682 (1997-11-01), Peasley et al.
patent: 5908176 (1999-06-01), Gilyard
patent: 6189836 (2001-02-01), Gold et al.
patent: 6763325 (2004-07-01), Stone
patent: 2002/0055086 (2002-05-01), Hodgetts et al.
patent: 2002/0128806 (2002-09-01), Anderson et al.
patent: 2002/0140696 (2002-10-01), Futamura et al.
patent: 2003/0211806 (2003-11-01), Paterson
Hall et al., “X-33 Attitude contro using the XRS-2200 Linear aerospike Engine”, American Institute of Aeronautics and Astronautics, 1998.
Stevenson et al., “Real time aircraft simulation using J-Mass”, IEEE 1995.
Lee & Hayes PLLC
Thangavelu Kandasamy
The Boeing Company
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