[go: up one dir, main page]

Russell et al., 1956 - Google Patents

A Flight Investigation of the Handling Characteristics of a Fighter Airplane Controlled Through a Rate Type of Automatic Control System

Russell et al., 1956

View PDF
Document ID
690144445180168841
Author
Russell W
Alford W
Sjoberg S
Publication year

External Links

Snippet

SUMMARY A flight investigation was made to obtain experimental information on the handling qualities of a fighter airplane which a pilot controlled by supplying signals to a rate type of automatic control system. A control stick which was similar to a conventional type of …
Continue reading at ntrs.nasa.gov (PDF) (other versions)

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/042—Control of altitude or depth specially adapted for aircraft
    • G05D1/046—Control of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for

Similar Documents

Publication Publication Date Title
US4094479A (en) Side slip angle command SCAS for aircraft
US3711042A (en) Aircraft control system
Anderson An examination of handling qualities criteria for V/STOL aircraft
EP0290532B1 (en) Synthetic speed stability flight control system
US4266743A (en) Pitch attitude stabilization system utilizing engine pressure ratio feedback signals
Russell et al. A Flight Investigation of the Handling Characteristics of a Fighter Airplane Controlled Through a Rate Type of Automatic Control System
BURCHAM, JR et al. Flight testing and simulation of an F-15 airplane using throttles for flight control
Tomczyk Aircraft maneuverability improvement by direct lift control system application
BERRY et al. Flying Qualities of a Large, Supersonic Aircraft in Cruise and Landing Approach
Franklin et al. Flight-path and airspeed control during landing approach for powered-lift aircraft
Sjoberg et al. A Flight Investigation of the Handling Characteristics of a Fighter Airplane Controlled Through an Attitude Type of Automatic Pilot
Williams Some recent research on the handling qualities of airplanes
Sim et al. Flight characteristics of the AD-1 oblique-wing research aircraft
Wolowicz et al. Summary of stability and control characteristics of the XB-70 airplane
CARLSON Direct sideforce control for improved weapon delivery accuracy
Gilyard et al. Results from flight and simulator studies of a Mach 3 cruise longitudinal autopilot
Gilyard et al. Development and flight test results of an autothrottle control system at Mach 3 cruise
Russell et al. Flight Investigations of Automatic Stabilization of an Airplane Having Static Longitudinal Instability
Lee et al. LAMS B-52 flight experiments in direct lift control
Franklin et al. Flight evaluation of stabilization and command augmentation system concepts and cockpit displays during approach and landing of powered-lift STOL aircraft
Quigley A flight and simulator study of directional augmentation criteria for a four-propellered STOL airplane
Boothe et al. Direct side force control for STOL crosswind landings
Painter AD-1 oblique wing research aircraft pilot evaluation program
Russell et al. Flight Investigation of a Centrally Located Rigid Force Control Stick Used with Electronic Control Systems in a Fighter Airplane
Innis et al. A flight and simulator study of directional augmentation criteria for a four-propellered STOL airplane