Schweikhard, 1967 - Google Patents
A method for in-flight measurement of ground effect on fixed-wing aircraft.Schweikhard, 1967
- Document ID
- 8944547192638792837
- Author
- Schweikhard W
- Publication year
- Publication venue
- Journal of Aircraft
External Links
Snippet
HISTORICALLY, as the Mach number of modern high-speed aircraft increases, so do the take-off and landing speeds and the associated ground runs. Since runway lengths cannot increase indefinitely, it is appropriate that every possible means of reducing these speeds …
- 230000000694 effects 0 title abstract description 52
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
-
- 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
-
- 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
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
- G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
- G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Nelson | Flight stability and automatic control | |
RU2615220C1 (en) | Method of determination of the control signal on the corner of the roll model of the hyperpower vehicle equipment (hve) for monitoring the aerodynamic identity on the reinolds number of trajectories of the flight of the model and the nuclear article when conducting anti-state aircraft research | |
Nicolosi et al. | Stability, flying qualities and longitudinal parameter estimation of a twin-engine CS-23 certified light aircraft | |
Larrabee et al. | Wind field estimation in UAV formation flight | |
Gonzalez-Rocha et al. | Measuring atmospheric winds from quadrotor motion | |
Araujo-Estrada et al. | Bio-inspired distributed strain and airflow sensing for small unmanned air vehicle flight control | |
Bunker | Turbulence and shearing stresses measured over the North Atlantic Ocean by an airplane-acceleration technique | |
Schweikhard | A method for in-flight measurement of ground effect on fixed-wing aircraft. | |
Gong et al. | Development of an in-flight thrust measurement system for UAVs | |
Chang et al. | Effect of sink rate on ground effect of low-aspect-ratio wings | |
Holley et al. | Wind modeling and lateral control for automatic landing | |
Nicolosi et al. | Flight tests, performances, and flight certification of a twin-engine light aircraft | |
Milenković-Babić et al. | Longitudinal stability characteristics of the LASTA airplane | |
Campos | On the influence of atmospheric disturbances on aircraft aerodynamics | |
Curry et al. | An in-flight investigation of ground effect on a forward-swept wing airplane | |
Zarovsky et al. | Flight Investigation of a Roll-Stabilized Missile Configuration at Varying Angles of Attack at Mach Numbers Between 0.8 and 1.79 | |
Rhyne | Flight assessment of an atmospheric turbulence measurement system with emphasis on long wavelengths | |
Tosti et al. | Hovering Flight Tests of a Four-Engine-Transport Vertical Take-Off Airplane Model Utilizing a Large Flap and Extensible Vanes for Redirecting the Propeller Slipstream | |
Payne | A flight investigation of some effects of automatic control on gust loads | |
Weng et al. | Analysis of dynamic ground effect for a jet transport in crosswind | |
van der Sman et al. | Incremental Nonlinear Dynamic Inversion and Multihole Pressure Probes for Disturbance Rejection Control of Fixed-wing Micro Air Vehicles | |
Zhenxing et al. | Air Data Estimation Based on Adaptive Kalman Filter | |
Sekino et al. | A flow-field integrated flight control: dynamic wind tunnel testing and simulation | |
Morgan et al. | Some Applications of Detailed Wind Profile Data to Launch Vehicle Response Problems | |
Papež et al. | Experimental method for unmanned aerial vehicles |