Development of mathematical model for the autonomous gliding delivery system

• Autorzy: Loroch L. , Sibilski K. , Żyluk A.
• Konferencja: Problemy Rozwoju, Produkcji i Eksploatacji Techniki Uzbrojenia / XV Konferencja Naukowo - Techniczna (XV; maj 2006; Rynia, Polska)
• Języki publikacji: EN

Abstrakty

EN

For parafoil and payload aircraft, control is affected by changing the length of several rigging lines connected to the outboard side and rear of the parafoil leading to complex changes in the shape and orientation of the lifting surface. Flight mechanics of parafoil and payload aircraft most often employ a 6 or 9 DOF representation with the canopy modeled as a rigid body during flight. The effect of control inputs usually is idealized by the deflection of parafoil brakes on the left and right side of the parafoil. This work focused on description of a 9 DOF parafoil and payload aircraft simulation model.

Słowa kluczowe

EN

mathematical models

PL

modele matematyczne

• Wydawca: Wojskowy Instytut Techniczny Uzbrojenia
• Czasopismo: Problemy Techniki Uzbrojenia
• Rocznik: 2006
• Tom: R. 35, z. 97
• Strony: 149--162
• Opis fizyczny: Bibliogr. 22 poz., rys.

Twórcy

autor

Loroch L.

autor

Sibilski K.

autor

Żyluk A.

• Instytut Techniczny Wojsk Lotniczych

Bibliografia

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