Spacecraft magnetic attitude control using approximating sequence Riccati equations

Rodriquez-Vazquez Antonio L.; Martin-Prats Maria A.; Bernelli-Zazzera Franco

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Spacecraft magnetic attitude control using approximating sequence Riccati equations

机译：使用近似序列Riccati方程的航天器磁姿态控制

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This paper presents the results of a spacecraft attitude control system based on magnetic actuators designed for low Earth orbits. The control system is designed by using a nonlinear control technique based on the approximating sequence of Riccati equations. The behavior of the satellite is discussed under perturbations and model uncertainties. Simulation results are presented when the control system is able to guide the spacecraft to the desired attitude in a variety of different conditions.

机译：本文介绍了基于为低地球轨道设计的磁致动器的航天器姿态控制系统的结果。通过使用基于Riccati方程的近似序列的非线性控制技术来设计控制系统。在摄动和模型不确定性下讨论了卫星的行为。当控制系统能够在各种不同条件下将航天器引导至所需姿态时，将给出仿真结果。

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《Aerospace and Electronic Systems, IEEE Transactions on》 |2015年第4期|3374-3385|共12页
作者
Rodriquez-Vazquez Antonio L.; Martin-Prats Maria A.; Bernelli-Zazzera Franco;
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Universidad de Sevilla, Departamento de Ingeniería Electrónica, Av. de los Descubrimientos S/N, 41092 Spain;

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正文语种 eng
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1. Spacecraft attitude control via a combined state-dependent Riccati equation and adaptive neuro-fuzzv approach [J] . Mohammad Abdelrahman, Sang-Young Park Aerospace science and technology . 2013,第1期

机译：通过状态相关的Riccati方程和自适应神经模糊方法相结合的航天器姿态控制
2. Magnetic torque attitude control of a satellite using the state-dependent Riccati equation technique [J] . Mohammad Abdelrahman, Insu Chang, Sang-Young Park International journal of non-linear mechanics . 2011,第5期

机译：基于状态的Riccati方程技术的卫星磁转矩姿态控制
3. Hardware-In-the-Loop Simulations of spacecraft attitude synchronization using the State-Dependent Riccati Equation technique [J] . Junoh Jung, Sang-Young Park, Sung-Woo Kim, Advances in space research . 2013,第3期

机译：使用状态相关的Riccati方程技术进行航天器姿态同步的硬件在环仿真
4. Optimized State-Dependent Riccati Equation Method for Spacecraft Attitude Estimation and Control [C] . L. Haim, D.Choukroun AIAA guidance, navigation, and control conference . 2012

机译：优化的状态相关Riccati方程法用于航天器姿态估计和控制
5. Algorithms and Optimal Control for Spacecraft Magnetic Attitude Maneuvers [D] . Desouky, Mohammed. 2019

机译：航天器磁姿态操纵的算法和最优控制
6. A note on improved F-expansion method combined with Riccati equation applied to nonlinear evolution equations [O] . Md. Shafiqul Islam, Kamruzzaman Khan, M. Ali Akbar, 2014

机译：改进的F展开方法与Riccati方程组合用于非线性发展方程的注释
7. An Efficient Algorithm for Periodic Riccati Equation for Spacecraft Attitude Control Using Magnetic Torques [O] . Yang, Yaguang 2016

机译：一种有效的航天器周期Riccati方程算法使用磁力矩控制姿态
8. Study to develop the equations describing the characteristics of rate and attitude sensors associated with spacecraft control systems [R] . Clair, J. 1966

机译：研究开发描述与航天器控制系统相关的速率和姿态传感器特性的方程

Spacecraft magnetic attitude control using approximating sequence Riccati equations

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