National Repository of Grey Literature 38 records found  previous11 - 20nextend  jump to record: Search took 0.01 seconds. 
Low Visibility Procedures
Kürthy, Peter ; Imriš, Pavel (referee) ; Vašíková, Kateřina (advisor)
This thesis deals with low visibility procedures and their direct application to airports, aircrafts, and aircraft operators. The main objective was to characterize the low visibility procedures as a file of conditions for airport equipment, aircraft equipment, skills and qualifications of the flight crew, and operating procedures. The work also raises the importance of analysis in terms of low visibility procedures in which the take-off, approach, and landing can be proceeded. A secondary objective was to cut the low visibility procedures requirements out of its basic form and convert it through practical application into a more comprehensible form. The result is an overview of the low visibility procedures for a point of view from both amateur and professional stand.
Production Building in Brno - Řečkovice
Horut, Jakub ; Jeneš, Rostislav (referee) ; Podroužková, Božena (advisor)
The design of the monolithic reinforced concrete horizontal supporting structures on the first deck above of a three-storey building is the aim of this bachelor thesis. Horizontal supporting structures consist of continuous slab of three fields heralded by girders in the longitudinal direction. In the static calculation, there are the ceiling slab, one girder, two angled slabs of staircase and the landing designed and evaluated. Structure was designed to fulfill especially functionality and to be economical. The drawings are the part of the work.
Alternative ways to take off and land for fixed-wing aircrafts
Cäsar, Tomáš ; Matějů, Jiří (referee) ; Zikmund, Pavel (advisor)
Target of this thesis was to propose and evaluate workability in matter of basic physical principles for shortening lengths of take-off and landing distances especially for small, single-seated aircrafts. These variants were proposed in order to be used at building roofs for transport of employees to work and back. Every variant is presented with loads, which would affect aircraft and pilot and also estimated runway length for comparison with classic landing. Calculations were made for two versions of aircrafts, one for present, achievable with current technologies and second futuristic, which takes into account expected development in aviation.
Comparison of traditional aeronautical precise approach navigation systems efficiencies with that of the LADGPS
Válek, David ; Sklenář, Filip (referee) ; Vosecký, Slavomír (advisor)
This work deals with the possibilities of using technologies and means of satellite navigation in civil air transport, focusing on the precise instrument approach of transport aircraft. The work describes traditional systems for guiding aircraft in the final phase of flight, their characteristics, principles of operation, advantages and disadvantages. Similarly, satellite navigation technology and its subsystems are described, which contribute to improving the accuracy and safety of these guidance devices. By analysing the characteristics and efficiency of all devices, a conclusion has been reached that the guidance technology could take hold in the future.
History of Civil Aviation 1970-2000
Zubrvalčík, Jan ; Šplíchal, Miroslav (referee) ; Chlebek, Jiří (advisor)
The main aim of this bachelor‘s thesis is utilize consice summary of history of civil aviation between year 1970 to 2000 and compare their performance. This era is typical with out-set of airplanes with large capacity and new construction solutions. This thesis is focused on planes for long distance with large capacity, but also on planes for middle and short distances too. Thesis is divided by range of airplanes and special charter is about supersonic civil planes.
Evaluation of the pilot's stress level during landing using a wearable electronics
Muschalik, David ; Sklenář, Filip (referee) ; Šplíchal, Miroslav (advisor)
The thesis focuses on the possibilities of objective stress measurement. It chooses parameters that are suitable for measurement by commonly available wearable electronics. It establishes a methodology for measuring stress using these devices, which it then verifies by conducting experiments with flight school students. It serves as proof of concept for similar measurements in further research or in flight schools.
High-lift system of the competition model aircraft
Vrba, Martin ; Koštial, Rostislav (referee) ; Koutník, Tomáš (advisor)
This Bachelor thesis is focused on compiling a summary of lift mechanization, at both the leading and the trailing edges used on plane models and unmanned means of transport. It briefly explains their principles and functions. It describes the method of calculation of the flight mode design of the competing aircraft according to the specifications of the Air Cargo Challenge competition.
Controlled Landing of an Autonomous Drone
Hraško, Andrej ; Barták, Roman (advisor) ; Obdržálek, David (referee)
The goal of this work is to develop and implement a desing for the most appropriate method allowing autonomous landing of the quadrocopter on a heliport with a visible pattern. This work includes an analysis dedicated to finding the best pattern for the designated landing area and the most reliable way to identify this pattern in an image taken from the camera of quadrocopter. The work explains the different ways of controlling devices as dynamic systems and implements algorithms for navigation of the quadrocopter to the target. The achieved results are verified by documented experiments. Powered by TCPDF (www.tcpdf.org)
Reinforced concrete slab supported on columns
Hlavička, Martin ; Šulák, Pavel (referee) ; Požár, Michal (advisor)
The thesis deals with the practical design and assessment of monolitic, reinforced-concrete flat slab. We focus on particular sections of the object, which are then characterized by moment coefficient method and finite element method using SCIA Engineer 19.1 software. Both ultimate limit state and service limit state are evaluated as well. After that we also focused on foundation (pile head plates), selected columns both outside and at the edges of the object, and staircase. The final ouput of this work is data accompanying report, static calculation and technical drawings of the object.
Evaluation of the pilot's stress level during landing using a wearable electronics
Muschalik, David ; Sklenář, Filip (referee) ; Šplíchal, Miroslav (advisor)
The thesis focuses on the possibilities of objective stress measurement. It chooses parameters that are suitable for measurement by commonly available wearable electronics. It establishes a methodology for measuring stress using these devices, which it then verifies by conducting experiments with flight school students. It serves as proof of concept for similar measurements in further research or in flight schools.

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