22nd Congress of International Council of the Aeronautical Sciences, Harrogate, UK, 28 August - 1st September, 2000
Paper ICAS 2000-4.10.4
PATH-ATTITUDE INCONSONANCE IN HIGH SPEED FLIGHT AND RELATED PATH CONTROL ISSUES
R. Stich (1), G. Sachs (1), T.H. Cox (2)
(1) Technische Universität München, Munich, Germany;
(2) NASA Dryden Flight Research Center, Edwards AFB, USA
Keywords: hypersonic flight, longitudinal dynamics, path-attitude lag, handling qualities,
simulator experiments
This paper presents results of a joint research
effort of NASA Dryden Flight Research Center
and the Institute of Flight Mechanics and Flight
Control of Technische Universität München on
longitudinal flight dynamics at hypersonic speeds.
At high speeds a large time lag between
pitch attitude and flight path angle exists. The
mechanisms which cause this path-attitude decoupling
are described. It will be shown further
that an limiting effect exists.
An “aggressive stick” piloting technique to
avoid the shortcomings of the path-attitude lag
is described. This type of control is also effective
to stabilize phugoid.
The simulation facility of Dryden Flight
Research Center which was used in the evaluation
is described. Simulation results concerning
the effect of path-attitude lag on “aggressive
stick” technique, of time delay and scaling of
vertical speed information are presented. Furthermore
results of flight tests with SR-71 and
Tu-144 at high supersonic speeds for similar
topics are presented.
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