Spacecraft attitude controller design for large angele maneuver using quaternio and d ual model control

机译：基于四元模型和对偶模型控制的大天使机动航天器姿态控制器设计

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In this paper, a new control structure for spacecraft attitude control, which consists of quanternion feedback and dual model control, is proposed. The quaternoion feedback rapidly reorients spacecraft and the dual mode control solver the tradeoff between thr fuel consumption and the accuracy. The duaol mode consists of PWPF(Pulse wideth Puulse Fequecy) modulator a nd Schmitt trigger. PWPF is used for the coarse control and Schmitt trigger for the fine control. For the proposed contrl scheme, stablity analysis is given and the performance is shown via simulation.

机译：本文提出了一种新的航天器姿态控制控制结构，该结构包括量子反馈和对偶模型控制。四元数反馈快速调整航天器和双模控制求解器的方向，从而在燃料消耗和精度之间进行权衡。 duaol模式由PWPF（脉冲宽度Puulse频率）调制器和施密特触发器组成。 PWPF用于粗调，施密特触发器用于细调。对于提出的控制方案，给出了稳定性分析并通过仿真显示了性能。

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来源
《4th IFAC(International Federation of Automatic Control) Symposium on Automatic Control in Aerospace 1998 Seoul, Korea, 24-28 August 1998》|1998年|p.301-305|共5页
会议地点 Seoul(KR)
作者
Hun-Sung Nam; Eung-Hwan Kim; Chanho Song;
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原文格式 PDF
正文语种 eng
中图分类航空、航天技术的研究与探索;
关键词
spacecraft Attitude Control; Quaternion Feedback; Dual Mode Control; PWPF(Pulse wideth Pulse Frequency) Modulator; Schmitt Trigger;

机译：航天器的姿态控制；四元数反馈；双模式控制； PWPF（脉冲宽度脉冲频率）调制器；施密特触发器;

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专利

1. Sliding-mode controller design for spacecraft attitude tracking maneuvers [J] . Chen Y.-P., Lo S.-C. IEEE Transactions on Aerospace and Electronic Systems . 1993,第4期

机译：航天器姿态跟踪机动的滑模控制器设计
2. Comments on “Quasi-Continuous Higher Order Sliding-Mode Controllers for Spacecraft-Attitude-Tracking Maneuvers” [J] . Ma K. Industrial Electronics, IEEE Transactions on . 2013,第7期

机译：关于“用于航天器姿态跟踪操纵的准连续高阶滑模控制器”的评论
3. Quasi-Continuous Higher Order Sliding-Mode Controllers for Spacecraft-Attitude-Tracking Maneuvers [J] . Pukdeboon C., Zinober A.S.I., Thein M.-W.L. Industrial Electronics, IEEE Transactions on . 2010,第4期

机译：航天器姿态跟踪机动的准连续高阶滑模控制器
4. Spacecraft attitude controller design for large angele maneuver using quaternio and d ual model control [C] . Hun-Sung Nam, Eung-Hwan Kim, Chanho Song International Federation of Automatic Control symposium on automatic control in aerospace . 1999

机译：使用Quaternio和D UAL模型控制的大型瓦尔对机动的航天器姿态控制器设计
5. Design of robust controllers for spacecraft maneuvers using state sensitivities. [D] . Liu, Shin-Whar. 1996

机译：使用状态敏感度的航天器操纵鲁棒控制器的设计。
6. On the Design of Hyperstable Feedback Controllers for a Class of Parameterized Nonlinearities. Two Application Examples for Controlling Epidemic Models [O] . Manuel De la Sen 2019

机译：一类参数化非线性的超稳定反馈控制器的设计。控制流行病模型的两个应用示例
7. Quasi-Continuous Higher Order Sliding-Mode Controllers for Spacecraft-Attitude-Tracking Maneuvers [O] . C. Pukdeboon, A.S.I. Zinober, M.-W.L. Thein 2010

机译：用于航天器 - 姿态跟踪机动的准连续高级滑模控制器
8. Modeling Attitude Dynamics in Simulink: A Study of the Rotational and Translational Motion of a Spacecraft Given Torques and Impulses Generated by RMS Hand Controllers [R] . Mauldin, R. H. 2010

机译：simulink中的姿态动力学建模：由Rms手控器产生的扭矩和脉冲的航天器旋转和平移运动的研究

Spacecraft attitude controller design for large angele maneuver using quaternio and d ual model control

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