Flight Investigation and Theory of Direct Side-Force Control
1979; American Institute of Aeronautics and Astronautics; Volume: 2; Issue: 6 Linguagem: Inglês
10.2514/3.55911
ISSN0162-3192
AutoresW. Brian Binnie, Robert F. Stengelf,
Tópico(s)Air Traffic Management and Optimization
ResumoSeveral side-force command modes were tested in Princeton's six-degree-of-freedom (6-DOF) variableresponse research aircraft (VRA), emphasizing the requirements of crosswind landing and lateral offset nulling. Pilot input modes included proportional and rate thumb switch, lateral stick, and foot pedal motions to command pure lateral acceleration, pure sideslip angle, and flat-turn maneuvers. Flight test results and supporting theoretical development are presented here. It is shown that a third-order dynamic model can be used to define control surface interconnects for decoupled side-force commands. Pilots' opinions regarding desirable command modes for the landing approach were shaped by their primary flying experience, although there was consensus that side-force commands that are uncoupled from conventional control inputs are preferred.
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