Set-valued estimators for Uncertain Linear Parameter-Varying systems

Silvestre, Daniel

doi:10.1016/j.sysconle.2022.105311

Cited by 4 publications

(1 citation statement)

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“…В СУ обертального руху ракети можуть мати місце суттєві відхилення коефіцієнтів моделі від номінальних величин, тому для підвищення ефективності використання методу заморожених коефіцієнтів [1] розроблений алгоритм їх уточнення шляхом використання даних вимірювання частини координат вектору стану [9]. Алгоритми уточнення параметрів ЛНС для різних варіантів збурень описані також у роботах [10][11][12][13].…”

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Dynamic Characteristics of Time-Varying Control System of the Rocket’s Rotational Movement

Avdieiev

2024

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The rocket motion control system is time-varying, because its parameters during flight depend on the trajectory point and fuel consumptions. In the available sources, due attention is not paid to the development of a mathematical apparatus of an applied value for the quan- titative assessment of the dynamic characteristics of a time-varying system. The purpose of the work is to justify the possibility of an algorithm building for calcu- lating the parameters of a link with constant parameters, which is equivalent to a time- varying system in terms of dynamic characteristics at the selected trajectory section. The link’s parameters are found by using the criterion of equivalence of the array of values of the motion model’soutput signal and the analytical solution of the link’s differential equation for a given sequence of input signals. This makes it possible to use the mathematical apparatus of stationary systems to determine the indicators of the disturbances compensation. The model of the control system of the rocket’s rotational movement in one plane is taken as a linear differential equation with time-varying parameters without taking into ac- count the executive device inertia and other disturbances. The link with constant parameters is a fractional-rational function of the second order, for the determination of which a se- quence of signals is applied to the input of the system model, the duration of which depends on the desired stability margin on the roots plane of the characteristic polynomial. Using the example of a time-varying system for controlling the rocket’srotational movement in the yaw plane, the possibility of determining the parameters of the transition process of compensation for the disturbances characteristic of it is shown for the selected tra- jectory section. The obtained results can be used in the design of a motion control system with time- varying parameters. The next stage of the research is an assessment of the complexity level of the calcula- tion algorithm when increasing the order of the system’smathematical model.

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