Flight Physics in Micro Air Vehicles and in Nature Final Report of Workshop AVT 182 RTO TECHNICAL MEMORANDUM RTO TM AVT 182

Date

2012-01-01

Author

OL, Michael
BERAN, P
RADESPİEL, R
Kurtuluş, Dilek Funda
WATKİNS, S
RİVAL, D
YUAN, W
LUCBOUHALİ, A
KONRATH, R
TROPEA, C
VOERSMANN, P
WOLF, T
IOSİLEVSKİ, G
LENTİNK, D
RUİJSİNK, R
BAYRAK, M
CAYLAR, S
ICEN, T
TEMİZ, K
VARDAR, K
BABİNSKY, H
BOMPHREY, R
JONES, C
SİBİLSKİ, K

Metadata

Show full item record

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Item Usage Stats

81
views

0
downloads

URI

https://hdl.handle.net/11511/70324

Collections

Department of Aerospace Engineering, Book / Book chapter

Suggestions

OpenMETU
Core

Flight mechanics of spin stabilized bodies and simulation. Bilgin, Engin; Department of Aeronautical Engineering (1988)
Flight Control System Design and Integration for a Small UAV Test Bed Tekinalp, Ozan; Yavrucuk, İlkay (null; 2009-08-17)
Flight Network-Based Approach for Integrated Airline Recovery with Cruise Speed Control ARIKAN, Ugur; Gürel, Sinan; Akturk, M. Selim (2017-11-01) Airline schedules are generally tight and fragile to disruptions. Disruptions can have severe effects on existing aircraft routings, crew pairings, and passenger itineraries that lead to high delay and recovery costs. A recovery approach should integrate the recovery decisions for all entities (aircraft, crew, passengers) in the system as recovery decisions about an entity directly affect the others' schedules. Because of the size of airline flight networks and the requirement for quick recovery decisions, ...
Flight control system design for an over actuated UAV against actuator failures Işık, Sinem; Tekinalp, Ozan; Department of Aerospace Engineering (2010) This thesis describes the automatic flight control systems designed for a conventional and an over actuated unmanned air vehicle (UAV). A nonlinear simulation model including the flight mechanics equations together with the interpolated nonlinear aerodynamics, environmental effects, mass-inertia properties, thrust calculations and actuator dynamics is created; trim and linearization codes are developed. Automatic flight control system of the conventional UAV is designed by using both classical and robust co...
Wing in ground effect vehicle: modelling and control Ghafoor, Abdul; Leblebicioğlu, Mehmet Kemal; Department of Electrical and Electronics Engineering (2015) The “Ground Effect” is the increase in the force which is acting on a lifting surface like wing, when it come to the close proximity of the ground. Ground effect vehicles (GEV) are the kind of amphibious vehicles that fly in close proximity of ground, making use of the aerodynamic interaction between the wings of the ground effect vehicle and ground (Sea or Earth surface) and it increases their efficiency 3-4 times more. There are many other advantages of the vehicles employing GE; they do not require a tak...

Citation Formats

M. OL et al., Flight Physics in Micro Air Vehicles and in Nature Final Report of Workshop AVT 182 RTO TECHNICAL MEMORANDUM RTO TM AVT 182. 2012.