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The purpose of this study was to gain a deeper understanding of the selection criteria used in preincubation programs. Particular focus has been placed on examining the exclusive and inclusive nature of these criteria, and how they relate to both egalitarian and utilitarian considerations.

The study used two data sources: archival available online data and semi-structured interviews. Forty-nine preincubation programs were examined, with 19 representatives interviewed. The data was analyzed using content analysis to understand the access and selection criteria applied at the preincubation stage.

The goals of preincubation programs vary, including developing students’ competencies, creating new companies or achieving the goals of the corporation that sponsored the program. preincubation programs use three levels of selection criteria, including entry criteria, the potential of the submitted idea and team and the personal characteristics and competencies of the applicants. The entry criteria varied across programs, with some programs being open only to university employees and students, while others were open to the public. The study found that the majority of preincubation programs used a combination of both egalitarian and utilitarian motivations in their selection criteria.

The criteria used to evaluate applications flowing into preincubation should be strongly related to the goals that preincubation is supposed to achieve. It is essential to consider that, contrary to previous knowledge, this process is not only aimed at supporting the creation of new businesses.

To the best of the author’s knowledge, this is the first study that analyzes the approach to selection criteria in preincubation programs with such diverse goals and in different countries as well as expanding the understanding of the criteria used at different stages of the incubation process and relating to the inclusiveness in entrepreneurship.

The purpose of this paper is to test the performance of the control system developed for the helicopter automatic approach and landing on the moving vessel deck, when different values of backlashes are applied to the four control actuators.

The system consists of automatic control algorithm based on the linear quadratic regulator and the vessel motion prediction algorithm based on autoregressive method with parameters calculated using Burg’s method. Necessary navigation data is provided by on-board inertial navigation system/Global Positioning System. Calculated control commands are executed by four electromechanical actuators. Performance of the mission, which is based on selected procedure of approach and landing of the helicopter on the moving vessel deck, is analyzed taking into account different values of backlashes applied to the actuators.

In this paper, a description of the control system dedicated for automatic approach and landing of the helicopter on the moving vessel deck is shown. Necessary information about helicopter dynamic model, control system and vessel motion model is included. Tests showing influence of actuator backlashes on the mission performance are presented.

The developed control methodology can be adapted for selected helicopter and used in prospective development of an automatic flight control system (AFCS) or in a simulator. The system can be used to define in which conditions helicopter can perform safe and successful automatic approach and landing on a moving vessel deck.

In this paper, an integrated control system is presented; influence of the control actuator backlashes on the mission performance is analyzed.