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Schierman et al., 2000 - Google Patents

On-line identification and nonlinear control of rotorcraft/external-load systems

Schierman et al., 2000

Document ID
10944233507949944431
Author
Schierman J
Ward D
Monaco J
Hull J
Lawrence T
Publication year
Publication venue
AIAA guidance, navigation, and control conference and exhibit

External Links

Snippet

There has been recent interest in improving helicopter flying qualities when the vehicle is carrying an external-load. This is widely regarded as a difficult operating condition, and will likely require an advanced control method. We propose here a model predictive control …
Continue reading at arc.aiaa.org (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
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control

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