Optimal Control of Spacecraft Motion in the Newtonian Gravitational Field: Application of Quaternions to Describe Orbit Orientation

Yu.N. Chelnokov

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Optimal Control of Spacecraft Motion in the Newtonian Gravitational Field: Application of Quaternions to Describe Orbit Orientation

机译：牛顿引力场中航天器运动的最优控制：四元数在描述轨道方向上的应用

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来源
《Космические исследования》 |1999年第4期|p.433-442|共10页
作者
Yu.N. Chelnokov;
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原文格式 PDF
正文语种 rus
中图分类航天（宇宙航行）;
关键词
spacecraft; optimal control; Newtonian Gravitational fields; orbit orientation;

机译：航天器最佳控制;牛顿引力场;轨道方向;

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专利

1. The Use of Quaternions in the Optimal Control Problems of Motion of the Center of Mass of a Spacecraft in a Newtonian Gravitational Field: III [J] . Yu. N. Chelnokov Cosmic research . 2003,第5期

机译：四元数在牛顿引力场中航天器质心运动的最佳控制问题中的应用：III
2. The Use of Quaternions in the Optimal Control Problems of Motion of the Center of Mass of a Spacecraft in a Newtonian Gravitational Field: Ⅱ [J] . Yu. N. Chelnokov Cosmic research . 2003,第1期

机译：四元数在牛顿引力场中航天器质心运动最优控制问题中的应用：Ⅱ
3. The use of quaternions in the optimal control problems of motion of the center of mass of a spacecraft in a Newtonian gravitational field. I. [J] . Yu.N.Chelnokov Космические исследования . 2001,第5期

机译：四元数在牛顿引力场中航天器质心运动的最佳控制问题中的使用。一世。
4. Boundary problem solution algorithm for the task of controlled spacecraft motion in irregular gravitational field of an asteroid [C] . Andrey Shornikov, Olga Starinova Russian-German conference on electric propulsions and their application . 2017

机译：界面问题对小行星不规则重力场的控制航天器运动任务的解决方案解决方案算法
5. The Equations of Motion of the Post-Newtonian Compact Binary Inspirals as Gravitational Radiation Sources Under the Effective Field Theory Formalism [D] . Yang, Zixin. 2020

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6. A New Quaternion-Based Kalman Filter for Human Body Motion Tracking Using the Second Estimator of the Optimal Quaternion Algorithm and the Joint Angle Constraint Method with Inertial and Magnetic Sensors [O] . Yingbo Duan, Xiaoyue Zhang, Zhibing Li 2020

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7. An optimal fuzzy PID control approach for docking maneuver of two spacecraft: Orientational motion [O] . A. Kosari, H. Jahanshahi, S.A. Razavi 2017

机译：两种航天器对接机动的最优模糊pID控制方法：方位运动
8. Visual Presentation of the Motion and Orientation of an Orbiting Spacecraft (Ogo) [R] . Mahoney, M., Quann, J. 1965

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Optimal Control of Spacecraft Motion in the Newtonian Gravitational Field: Application of Quaternions to Describe Orbit Orientation

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