Nowadays, the nature of the projects has changed to be unique, uncertain, ambiguous,complex and innovative. It becomes hard to plan in advance the project progress, asdeviations from plans and unpredictable changes occur more frequently. This can bespecifically observed in the software development industry which needs to constantlymeet customers’ rapidly changed requirements. Traditionally, software projects aredeveloped through a plan-driven approach which emphasizes an overall project plan andcontrol process in terms of project management. Recently, this has been challenged byagile approach that focuses on flexibility to quickly meet changing requirements, andthese new agile methods provoked huge interest and got more and more popular andwidely applied especially in IT industry. However, the popularity does not mean theagile methods have advantage over traditional plan-based project management methods.In fact, both methods have own advantages and disadvantages and cannot be fullyreplaced by each other. Therefore, it becomes important and necessary for companymanagement to know how to select a suitable method for the new software developmentproject to get the maximum benefits.The purpose of this study is to describe different project management methods(traditional plan-driven and agile methods) and their various consequences for themanagement of software-development projects. Additionally, a more practical purposeis to suggest on what grounds a choice between methods may be made. Morespecifically, this research aims to provide the possible solution on how to selecttraditional plan-driven or agile project management method for managing a newsoftware development project. The research conducted a qualitative study in a casecompany of IT industry through several semi-structured interviews and questionnaireswith experienced and knowledgeable employees. It started with the analysis andcomparison of traditional and agile project management methods’ characteristics andapplication domains based on two specific examples (PROPS and Scrum) selected fromtraditional and agile project management methods respectively, in order to identify a setof preliminary outstanding characteristics which could be used to help IT company tochoose project management methods for new software development projects. Theempirical data obtained from interviews of case company was investigated to verifythese characteristics based on the literature review, and further adjusted thecharacteristics identification. After going through the whole research process, finallyresearchers identified the most suitable characteristics that were important both intheory and practice to examine on what ground a software development company needsto base the selection of project management methods. These suitable characteristics are:Project Complexity, Communication, Competencies and Requirements, in order to helpselect the best management way for the specific project.

The thesis deals with aerodynamic characteristics identification from flight measurement. The topic is part of flight mechanic – handling qualities. The first theoretic part consists of three identification methods description: Error equation method, Output error method and Filter error method. Mathematical model of an airplane is defined and restricted to the motion with 3 degree of freedom. There is also introduced simulation of flight measurement for identification software validation. Practical part is focused on experiment preparation, execution and evaluation. The airplane VUT 700 Specto had been chosen to carry out flight tests. The airplane was modified to the new electric powered VUT 700e Specto after first measurement flights with combustion engine. Data record from on-board measurement unit was completed by telemetric data from autopilot and remote control system. Flight tests were carried out in stabilised mode of autopilot in symmetric flight. The results were confronted with analytical analysis results and DATCOM+ software parameter estimation.

The thesis deals with aerodynamic characteristics identification from flight measurement. The topic is part of flight mechanic – handling qualities. The first theoretic part consists of three identification methods description: Error equation method, Output error method and Filter error method. Mathematical model of an airplane is defined and restricted to the motion with 3 degree of freedom. There is also introduced simulation of flight measurement for identification software validation. Practical part is focused on experiment preparation, execution and evaluation. The airplane VUT 700 Specto had been chosen to carry out flight tests. The airplane was modified to the new electric powered VUT 700e Specto after first measurement flights with combustion engine. Data record from on-board measurement unit was completed by telemetric data from autopilot and remote control system. Flight tests were carried out in stabilised mode of autopilot in symmetric flight. The results were confronted with analytical analysis results and DATCOM+ software parameter estimation.