The use of groundspeed in combination with airspeed has been considered and shown to be an effective aid in the execution of an approach and landing in a heavy jet transport airplane. A flight dynamics analysis shows that the response of such aircraft to sudden changes in headwind is quite sluggish, requiring more than 100 seconds for equilibrium conditions to be regained in the worst case. A feasibility demonstration model of a radar-altimeter-based system for the measurement of groundspeed has been subjected to a limited in-flight evaluation. It is a self-contained unit requiring no ground-based equipment and no on-board equipment other than the small flush transmit and receive antennas and the associated cable runs. While the current unit does not meet the desired accuracy standard (delta = + or - 3 knots, or less), it approaches it at times, and greater accuracy can be achieved with further development. Responsiveness to rapidly changing groundspeed matched that of the reference inertial navigation system; and satisfactory groundspeed tracking was maintained during turning, climbing, and descending flight. (Author)
The Use of Groundspeed. in a Wind Shear and the Flight Evaluation of a Radar-Altimeter-Based System for the Measurement of Groundspeed
1981
44 pages
Report
Keine Angabe
Englisch
Aeronautics , Avionics , Dynamic Meteorology , Wind shear , Radio altimeters , Radar antennas , Jet transport aircraft , Aircraft antennas , Test and evaluation , Turning flight , Inertial navigation , Jet aircraft , Equilibrium(General) , Models , Flight , Tracking , Airspeed , Dynamics , Cables , Standards , Aircraft , Accuracy , Climbing , Groundspeed indicators , Flush antennas , Climbing flight , Descending flight
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