The process of designing autonomous vector measuring instrument is considered. The characteristic of autonomous vector measuring instruments applied in unmanned aviation is given. The concept of the smart measuring instrument concerning to the researched device is explained. The structure of information support for designing redundant nonorthogonal measuring instrument is given. The block-scheme of the process of designing redundant nonorthogonal configurations is represented. The process of choice of the optimal configuration of autonomous vector measuring instruments based on redundant nonorthogonal measuring bases is represented. The computer-aided designed procedures for optimal configuration choice are described. The basic algorithms necessary for functioning of the smart vector measuring instruments are listed. The example of the analysis of nonorthogonal configurations is represented. The obtained results are applicable in measuring systems of unmanned aviation. They also can be useful for other aerospace applications.

Features of development models and modeling of stabilization systems of ground vehicle equipment are considered. Features of the optimal synthesis procedure for the system of the considered type are mentioned. The main goal of the research is to study the design features of the stabilization system with the digital control unit. Two approaches to the discretization of a system with the digital control unit are given. Appropriate block-diagrams are represented. Analysis of sampling methods and appropriate software is given. Possible program realizations of transfer functions in a model of the digital control unit are discussed. Features of representation of digital filters unit are proposed. Modelling of the stabilization system with the digital control unit was carried out. Simulation results are represented. Transient processes on the angular rate with different ways of sampling are given. Results of the comparative analysis of different sampling ways are shown in the tabular form. The obtained results can be useful for designing control systems of the wide type.