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Analysis of Classical and Adaptive Control Algorithms for a Space Vehicle
Ist Teil von
2019 23rd International Conference on System Theory, Control and Computing (ICSTCC), 2019, p.827-832
Ort / Verlag
IEEE
Erscheinungsjahr
2019
Quelle
IEEE Electronic Library (IEL)
Beschreibungen/Notizen
This paper addresses the problem of modeling the dynamics of a launch vehicle and some control algorithms designed to ensure the stability of the closed-loop system and to meet certain performance requirements. The equations of motion were written taking into account the forces acting on a space launcher and the disturbances that may occur and lead to changes in the desired trajectory without taking into account the effects of nozzle dynamics, propellant motion and bending modes. The formulated structure is brought to state space representation and used in the design of the control algorithms. A comparative analysis of different classical control and adaptive algorithms (PD, PID, MRAC) was performed.