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

Caughey, 2011 - Google Patents

Introduction to aircraft stability and control course notes for M&AE 5070

Caughey, 2011

View PDF
Document ID
10122779939084770716
Author
Caughey D
Publication year
Publication venue
Sibley School of Mechanical & Aerospace Engineering Cornell University

External Links

Snippet

Flight dynamics deals principally with the response of aerospace vehicles to perturbations in their flight environments and to control inputs. In order to understand this response, it is necessary to characterize the aerodynamic and propulsive forces and moments acting on …
Continue reading at courses.cit.cornell.edu (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
    • G05D1/08—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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y02T50/16—Drag reduction by influencing airflow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • 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
Caughey Introduction to aircraft stability and control course notes for M&AE 5070
Vepa Flight dynamics, simulation, and control: for rigid and flexible aircraft
Etkin et al. Dynamics of flight: stability and control
Weisshaar et al. Aeroelastic tailoring for improved UAV performance
Shields et al. Roll stall for low-aspect-ratio wings
Dogan et al. Control and simulation of relative motion for aerial refueling in racetrack maneuvers
Iliff Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
Koloschin et al. Flight Physics of Fuel-Saving Formation Flight
López-Briones et al. Aerodynamic Analysis for the mathematical model of a dual-system UAV
Sharma et al. Simulation of maritime helicopter dynamics during approach to landing with time-accurate wind-over-deck
Hainline et al. Vehicle Design Study of a Straight Flying-Wing with Bell Shaped Spanload
Colgren et al. Effective design of highly maneuverable tailless aircraft
Morris Flight dynamic constraints in conceptual aircraft multidisciplinary analysis and design optimization
Green et al. CFD analysis of the F/A-18E super hornet during aircraft-carrier landing high-lift aerodynamic conditions
Karatoprak Sizing and optimization of the horizontal tail of a jet trainer
Denieul et al. Interactions of Aircraft Design and Control: Actuators Sizing and Optimization for an Unstable Blended Wing-Body
Chudoba et al. Trim Equations of Motion for Aircraft Design: Steady State Straight Line Flight
Amankwah A Three Degrees of Freedom (3DoF) Dynamic Modeling and Simulation of an Unmanned Aerial Vehicles
De Hart Advanced take-off and flight control algorithms for fixed wing unmanned aerial vehicles
Leishman Airplane Stability & Control
Mishra et al. Integrating Stability and Control Considerations into the Sizing of an Advanced Air Mobility VTOL Aircraft
Williams et al. Kites for Wind Energy
Phillips et al. Characteristic length and dynamic time scale associated with aircraft pitching motion
Hugo Autonomous landing of a fixed-Wing unmanned aircraft with partialwing and stabiliser losses
Lee et al. Autonomous flight control system design for a blended wing body