[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Krachmalnick et al., 1968 - Google Patents

Automatic flight control system for automatic terrain-following.

Krachmalnick et al., 1968

Document ID
12309414062169131046
Author
Krachmalnick F
Vetsch G
Wendl M
Publication year
Publication venue
Journal of Aircraft

External Links

Snippet

This paper discusses the design, simulation, and flight testing of an automatic flight control system (AFCS) developed under Project 666 At to provide an automatic terrain-folio wing capability in a supersonic, fighter-bomber type of aircraft. Functional operation and features …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0607Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0615Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0077Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements using redundant signals or controls
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/0055Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
    • G05D1/0061Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements for transition from automatic pilot to manual pilot and vice versa
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10Simultaneous control of position or course in three dimensions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/40Transmitting means with power amplification using fluid pressure
    • B64C13/42Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/04Initiating means actuated personally

Similar Documents

Publication Publication Date Title
LaCr Application of nonlinear systems inverses to automatic flight control design-System concepts and flight evaluations
US6041273A (en) Emergency control aircraft system using thrust modulation
US5330131A (en) Engines-only flight control system
US6102330A (en) Emergency multiengine aircraft system for lateral control using differential thrust control of wing engines
Kaneshige et al. Generic neural flight control and autopilot system
US4648569A (en) Airplane automatic control force trimming device for asymmetric engine failures
US3493836A (en) Static and dynamic failure monitor for aircraft automatic pilots
Burken et al. Flight-test results of propulsion-only emergency control system on MD-11 airplane
Krachmalnick et al. Automatic flight control system for automatic terrain-following.
Burken et al. Longitudinal emergency control system using thrust modulation demonstrated on an MD-11 airplane
US2833496A (en) Flight control system
Tremant Operational Experiences and Characteristics of the X-15 Flight Control System
Burken et al. Flight test of a propulsion-based emergency control system on the MD-11 airplane with emphasis on the lateral axis
STEWART Integrated flight propulsion control research results using the nasaf-15 hidec flight research facility
SWORTZEL et al. The fighter CCV program-Demonstrating new control methods for tactical aircraft
Steck et al. An advanced flight control system for general aviation application
Merkel et al. Development and evaluation of precision control modes for fighter aircraft
Hunter Survivable flight control system fly-by-wire development and flight test
Gilyard et al. Development and flight test results of an autothrottle control system at Mach 3 cruise
Ammons F-16 flight control system redundancy concepts
Doniger et al. Flight control techniques for advanced commercial transports
McMaster et al. Development of the F-12 aircraft flight control system
Flapper et al. L-1011 flight control system
JACKSON et al. Design and development of the primary fly-by-wire flight control system for the XV-4B V/STOL research aircraft
Gallagher et al. Flying qualities design of the Northrop YF-17 fighter prototypes