Analytical algorithm for constructing the orbital orientation of a spacecraft with an incomplete measurement of the state vector components

DOI10.1134/S1064230719040178zbMath1448.93089OpenAlexW3004915761MaRDI QIDQ786105

D. Kharzeev

Publication date: 12 August 2020

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230719040178

zbMATH Keywords

joint synthesismodal controller and observerrotational motion of spacecraft

Mathematics Subject Classification ID

Application models in control theory (93C95) Synthesis problems (93B50) Observers (93B53)

Related Items (2)

Reducing the problem of the modal control by output for stationary fourth-order systems with two inputs and two outputs to the control by state for a system with a single input ⋮ Analytical synthesis of an aircraft's lateral motion control by output at the lack of measurements of slip and roll angles

Cites Work

• Unnamed Item
• Output control of the longitudinal motion of a flying vehicle
• On the rapid orbital attitude control of manned and cargo spacecraft \textit{Soyuz MS} and \textit{Progress MS}
• Output control of a spacecraft motion spectrum
• Stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle: analytical synthesis

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