SUMMARY
Context. A method for obtaining estimates of the dependence of stability factor and reduced work during the transient processfor compensation of a constant disturbing acceleration on the presence in law of control data about current kinematic parameters ofthe executive device under condition of ensuring a prescribed static error is developed. It will give a possibility to take decision aboutlevel of complexity for appropriate units in stabilizing system.Objective. The purpose of the research is to estimate the influence of the law of control reduction by means of exclusion fromone the data about state vector of the executive device on requirements to its power and stability factor.Method. A linear stationary in the vicinity of a certain point of the trajectory model of a plane rotational motion of a rocket forspace purposes has been adopted, with taking into account the inertia of the executive device. Estimation of the stability factor iscarried out on the plane of the roots of the characteristic polynomial and two coefficients of the law of control. Divided to the squareof constant perturbation acceleration, the work of the executive device is determined by analytical solution of the differentialequations of perturbed rotational motion in one of the stabilization planes. For statically stable and unstable rocket the dependenceexamples of the named performances on coefficients of the law of control by coordinates of the state vector are made.Results. For the application of the rocket for space purposes for the first time the dependence of the named indices of stabilizingsystem on availability in the law of control data about angle of rotation of steering gear and its velocity is established.Conclusions. It is proven the ability of improvement the stabilizing system by means of inclusion in law of control kinematic parametersof the executive device from the point of view of such performances as a stability factor and energy costs during transientprocesses.