Accession Number : ADA456829


Title :   Scaling Flight Tests of Unmanned Air Vehicles


Descriptive Note : Master's thesis


Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING AND MANAGEMENT


Personal Author(s) : Abeygoonewardene, Jeevani I


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a456829.pdf


Report Date : Sep 2006


Pagination or Media Count : 107


Abstract : Increasing technological advances and research interest in unmanned air vehicles (UAVs), have led to the need for having safe, inexpensive and effective means of experimenting with their fight performance and surveillance capabilities. Work has previously been done in areas of controlling, analyzing, and predicting cooperative and autonomous operations of UAVs and other vehicles. In addition, there are well established guidelines for scaling experiments in fluid mechanics, where geometric, kinematic and dynamic similarity is obtained by formulating problems in terms of non dimensional variables using dimensional analysis. However, little or no work has been done in developing experiments or guidelines for air vehicles and their sensors. The currently available experiments for such purposes, which are designed around commercially available equipment, have not been standardized and cannot be related to the real systems and the real requirements. The analysis done in this research provides an important step in setting up guidelines for experimental scaling of flight tests of UAVs. This makes it possible to use computer simulations and ground hardware experiments in a useful way for performance evaluations before having to fly the actual vehicle. Equations and simulations used have been defined in non-dimensional terms in order to allow for a scale independent approach as per the Buckingham Pi theorem. Comparisons have been drawn of flight and sensor performance characteristics between a nominal wide search area vehicle and two surrogate hardware systems having widely varying operating characteristics.


Descriptors :   *FLIGHT TESTING , *AIRCRAFT , *UNMANNED , TEST AND EVALUATION , PERFORMANCE(ENGINEERING) , SELF OPERATION , SURVEILLANCE , FLUID MECHANICS , EQUATIONS , SCALE , THESES , COMPUTERIZED SIMULATION , REQUIREMENTS


Subject Categories : Aerodynamics
      Pilotless Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE