Effects of Mass and Size on Control of Large Receiver in Aerial Refueling

Atilla Dogan, Christopher M. Elliott, Fransell Riley, William Blake

AIAA Atmospheric Flight Mechanics Conference · 2009 · 17 citations · 4 references

Concepts

Abstract

This paper presents the research work conducted to study the ability of a large receiver aircraft with two difierent size and three difierent mass conflgurations to maneuver and maintain contact position behind a KC-135 tanker in the presence of atmospheric turbulence. An LQR controller was used for the inner loop control system. The ∞ight track that was simulated was taken from 2004 testing of a Learjet behind a KC-135 that was part of the AFRL AAR program and includes signiflcant winds at altitude.

References

4