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Energetics of free and tethered flight in bumblebees (<i>Bombus terrestris</i>, Linnaeus 1758). [PDF]
Biol LettSenior EJ +3 more
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Comparisons of AEROX computer program predictions of lift and induced drag with flight test data
John A. Axelson, G. C. Hill
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Mariner 9 data storage subsystem flight performance summary
Nicholas E. Thomas, B. T. Larman
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IEEE Circuits and Devices Magazine, 2002
We discuss feasible design methods for implementing the reliable MIL-STD-1773 data buses that use mature optoelectronic devices. To guarantee reliable data transmission over the data bus, we present three efficient modulation techniques that can be used to reduce the complexity of optical transceivers and the processing time at each receiver, compared ...
null Jian-Guo Zhang +2 more
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We discuss feasible design methods for implementing the reliable MIL-STD-1773 data buses that use mature optoelectronic devices. To guarantee reliable data transmission over the data bus, we present three efficient modulation techniques that can be used to reduce the complexity of optical transceivers and the processing time at each receiver, compared ...
null Jian-Guo Zhang +2 more
openaire +1 more source
1999
Robust stability analysis considers the stability of a system subject to a set of modeling errors and perturbations represented by a norm bounded set △. A logical question that arises is how to reasonably determine this set. This issue is important for computing robust aeroservoelastic stability margins since μ may be overly conservative if the ...
Rick Lind, Marty Brenner
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Robust stability analysis considers the stability of a system subject to a set of modeling errors and perturbations represented by a norm bounded set △. A logical question that arises is how to reasonably determine this set. This issue is important for computing robust aeroservoelastic stability margins since μ may be overly conservative if the ...
Rick Lind, Marty Brenner
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IEEE Potentials, 1991
The calibration of measurements of the four critical parameters that define an aircraft's air data state, the state of an aircraft relative to the air mass through which it is flying, is discussed. The parameters are altitude, airspeed, angle-of-attack, and angle-of-sideslip.
D.K. Taniguchi, R.L. Hagrman
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The calibration of measurements of the four critical parameters that define an aircraft's air data state, the state of an aircraft relative to the air mass through which it is flying, is discussed. The parameters are altitude, airspeed, angle-of-attack, and angle-of-sideslip.
D.K. Taniguchi, R.L. Hagrman
openaire +1 more source