- Tytuł:
- Development of mathematical model for the autonomous gliding delivery system
- Autorzy:
-
Loroch, L.
Sibilski, K.
Żyluk, A. - Powiązania:
- https://bibliotekanauki.pl/articles/235504.pdf
- Data publikacji:
- 2006
- Wydawca:
- Wojskowy Instytut Techniczny Uzbrojenia
- Tematy:
-
modele matematyczne
mathematical models - Opis:
- 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.
- Źródło:
-
Problemy Techniki Uzbrojenia; 2006, R. 35, z. 97; 149-162
1230-3801 - Pojawia się w:
- Problemy Techniki Uzbrojenia
- Dostawca treści:
- Biblioteka Nauki
Artykuł