Abstract
The selection of the design parameters of a perspective flightpath display must take into account the operational capabilities of the vehicle to be controlled. As a result, designs of perspective flightpath displays that have been optimized for fixed-wing aircraft may need to be modified in order to be useful for advanced approach procedures with tiltrotors. This paper discusses potential changes that are required as a result of the different range of flightpath angles used in approach trajectories and the different range of velocities.
Original language | English |
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Journal | SAE Technical Papers |
DOIs | |
State | Published - 1999 |
Event | 1999 World Aviation Conference - San Francisco, CA, United States Duration: 19 Oct 1999 → 21 Oct 1999 |