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

TIEDEMAN et al., 1979 - Google Patents

Inertially augmented approach couplers[Final Report, Jun. 1975- Jun. 1979]

TIEDEMAN et al., 1979

Document ID
14396042405765509420
Author
TIEDEMAN D
BENSON F
MILLER L
RUDIG R
SCHULDT T
SHIH C
SKELLEY E
Publication year

External Links

Continue reading at scholar.google.com (other versions)

Classifications

    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • 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

Similar Documents

Publication Publication Date Title
GB1530245A (en) Helicopter apparatus
Burcham Jr et al. Development and flight test of an emergency flight control system using only engine thrust on an MD-11 transport airplane
TIEDEMAN et al. Inertially augmented approach couplers[Final Report, Jun. 1975- Jun. 1979]
Schroeder et al. Simulator platform motion effects on pilot-induced oscillation prediction
Deets HiMAT flight program: Test results and program assessment overview
US3089257A (en) Simulated on-ground aircraft pitching moment system
BAILEY, JR Development of a Side-Stick Controller for Aerospace Vehicles
Kempel et al. Flight Evaluation of HL-10 Lifting Body Handling Qualities at Mach Numbers from 0.30 to 1.86
REYNOLDS et al. Total In-Flight Simulator (TIFS)-A New Aircraft Design Tool
RANZ et al. Boeing 7 J 7 fly-by-wire control development
Simmons et al. Aviator visual performance: A comparative study of a helicopter simulator and the UH-1 helicopter
Aiken et al. Rotorcraft handling-qualities design criteria development
Tiedeman et al. Inertially Augmented Approach Couplers
Riley et al. Piloted simulation study of an ils approach of a twin-pusher business/commuter turboprop aircraft configuration
Aiken et al. A fixed-base ground simulator study of control and display requirements for VTOL instrument landings with a decelerating approach to a hover[Final Report]
Sinclair et al. In-flight simulation program at the NAE Flight Research Laboratory.
Hanke Flying qualities experiments of rate command/attitude hold systems in the HFB 320 in-flight simulator
KELLY et al. Simulator results of an F-14 A airplane utilizing an aileron-rudder interconnect during carrier approaches and landings[Progress Report, Jan. 1979- Feb. 1980]
Patterson Jr Criteria for determination of minimum usable approach speed.
Cheeseman Is the pilot necessary in a light observation helicopter?
HAY et al. Summary of Department of Transportation/Federal Aviation Administration task force on crew workload report[Final Report, May 1977- Aug. 1978]
SPADY et al. Flight management research utilizing an oculometer(pilot scanning behavior during simulated approach and landing)
Keller et al. Digital avionics system for the Shuttle Training Aircraft
Blatt Flight control system advances for near-future military aircraft
Sherman et al. Study of Exit Phase of Flight of a Very High Altitude Hypersonic Airplane by Means of a Pilot-controlled Analog Computer