Other

Basic information

Name MINOHARA, Tatsuo
Belonging department
Occupation name
researchmap researcher code
researchmap agency

Title

Display System for Control Configured Vehicle

Sole or Joint Author

Sole Author

Date of Issue

2004/10

Conference Presentation(name)

Proceedings of 23rd Digital Avionics Systems Conference, Salt lake city

Summary

In a helicopter or an airplane which has enhanced maneuverability by using active control technology, its nose vector can be directed at a wide angle with its velocity vector. Especially, the maneuvers of an airplane which has widely enhanced maneuverability, such as X-31 and Su-27 should be focused to rather than an usual CCV (Control Configured Vehicle) plane, such as X-29 and F-16 CCV.  Also in a space plane, such differences of angles are usually controlled and precisely used when docking or landing to the target station. Those angles of the vehicle should be indicated against the velocity vector and also against the target.  In addition to the indication of the angles, indicators of speeds and relative position against the target are required to direct side force control and direct lift control. In this paper, a display system in which fuselage pointing,  translation movements, and direct forces are indicated is proposed. Those indications will improve the recognition of maneuver for a pilot. This display system is currently virtually implemented in a simple flight simulator software.

Subject1

Subject2

Subject3