Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CONCHA R DE
Original Assignee
CONCHA R DE
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by CONCHA R DEfiledCriticalCONCHA R DE
Publication of GB1502789ApublicationCriticalpatent/GB1502789A/en
Investigation of the use of vectored thrust during carrier landings(Carrier landing characteristics of vectored- thrust aircraft obtained in piloted fixed-base flight simulator studies)
The development of an integrated flight guidance and control system for modern high- performance aircraft(VTOL aircraft fly by wire system eliminating errors automatically, discussing electronic and electrohydraulic control components, flight test model design, prototype, etc)
An automatic guidance concept for VTOL aircraft(V/STOL aircraft automatic flight control, guidance and navigation by onboard computer, discussing mathematical model and simulation results)
Direct lift control as a landing approach aid(Direct lift control as landing approach aid by providing more rapid means of changing and controlling flight path than conventional methods)
A system to vary the stability and control of a deflected-jet fixed-wing vtol aircraft(Variable stability system for vtol aircraft, allowing damping and control power to vary over range of flight characteristics)
Evaluation of in-flight simulation using a helicopter of variable stability and control with regard to its use as an auxiliary in aircraft development(Evaluation of in-flight simulation of flying platform using helicopter with variable stability and maneuverability)
The interaction of the analyzers under flight conditions on airplanes and spaceships(Interaction of visual, vestibular, and motor sense organs under simulated flight conditions)
VAK 191 B experimental program for a V/STOL Strike-Recce aircraft(Design, development, and flight characteristics of VAK 191 B V/STOL strike/reconnaissance aircraft)
Airport-area airspace used in simulated operations with an experimental powered-lift STOL airplane(Simulation tests of short takeoff transport aircraft to determine airport and air space requirements under normal operating conditions)
A discussion of the use of thrust for control of VTOL aircraft(Engine thrust vectoring and thrust modulation for control of V/STOL aircraft during hover)
Aerodynamic problems posed by the concept of a supersonic transport(Optimization of supersonic and subsonic cruise, slow speed flight and flying qualities of supersonic transports)