公开(公告)号：WO2018186907A1

公开(公告)日：2018-10-11

申请号：PCT/US2017/056309

申请日：2017-10-12

Applicant: RAYTHEON COMPANY

Inventor： KOESSLER, Jeffrey, H. ,  LEE, Anthony, O. ,  TRETSCHOK, Cody, D. ,  ARTZ, Gregory, J.

IPC: B64C3/38 ,  B64C17/00 ,  B64C39/00 ,  B64C39/02

CPC classification number: B64C3/38 ,  B64C1/22 ,  B64C1/26 ,  B64C17/02 ,  B64C39/008 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/10 ,  B64C2201/128 ,  B64C2201/165 ,  B64C2211/00

Abstract: A control system of a flight vehicle automatically varies the relationship between the center of gravity and the center of pressure of the flight vehicle. The control system automatically adjusts a center of pressure of the flight vehicle depending on a varying payload or payload type that is removably couplable to the flight vehicle. The control system automatically limits translational movement of the one or more wings of the flight vehicle in response to coupling of a payload to a fuselage of the flight vehicle.