Evaluation of Several Control/Display Concepts for V/STOL Shipboard Landing

Format:

Conference/Event

Author/Creator:

Donley, Shawn T., author.

Conference Name:

Aerospace Congress & Exposition (1980-10-13 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1980

Summary:

The relative merits of three flight control laws and two distinctly different Head-Up Display concepts have been evaluated in a piloted simulation for the task of landing a generic lift/cruise fan V/STOL aboard a DD-963 class destroyer. Results indicate that airwake turbulence in the vicinity of the landing pad dominates landing performance. A high level of vehicle augmentation, in the form of a translational relative velocity command/ relative position hold control law, was required to achieve acceptable pilot ratings in higher than 30 kts wind-over-deck conditions

Notes:

Vendor supplied data

Publisher Number:

801205

Access Restriction:

Restricted for use by site license