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Titlebook: Satellite Formation Flying; High Precision Guida S. Mathavaraj,Radhakant Padhi Book 2021 Springer Nature Singapore Pte Ltd. 2021 Satellite

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发表于 2025-3-21 18:41:59 | 显示全部楼层 |阅读模式
书目名称Satellite Formation Flying
副标题High Precision Guida
编辑S. Mathavaraj,Radhakant Padhi
视频video
概述Covers optimal as well as adaptive control strategy for high precision formation flying of small satellites.Presents detailed formulation along with merits and demerits of all the discussed approaches
图书封面Titlebook: Satellite Formation Flying; High Precision Guida S. Mathavaraj,Radhakant Padhi Book 2021 Springer Nature Singapore Pte Ltd. 2021 Satellite
描述Small satellite technology is opening up a new era in space exploration offering reduced cost of launch and maintenance, operational flexibility with on-orbit reconfiguration, redundancy etc. The true power of such missions can be harnessed only from close and precise formation flying of satellites. Formation flying missions support diverse application areas such as reconnaissance, remote sensing, solar observatory, deep space observatories, etc. A key component involved in formation flying is the guidance algorithm that should account for system nonlinearities and unknown disturbances. The main focus of this book is to present various nonlinear optimal control and adaptive guidance ideas to ensure precise close formation flying in presence of such difficulties. In addition to in-depth discussion of the relevant topics, MATLAB program files for the results included are also provided for the benefit of the readers. Since this book has concise information about the various guidance techniques, it will be  useful reference for researchers and practising engineers in the space field..
出版日期Book 2021
关键词Satellite Formation Flying; Optimal Control; Linear Quadratic Regulator; Nonlinear Control; Neuro-Adapti
版次1
doihttps://doi.org/10.1007/978-981-15-9631-5
isbn_softcover978-981-15-9633-9
isbn_ebook978-981-15-9631-5
copyrightSpringer Nature Singapore Pte Ltd. 2021
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发表于 2025-3-21 20:59:47 | 显示全部楼层
Infinite-Time LQR and SDRE for Satellite Formation Flying,flying is demonstrated in their respective validity regions. Both methods are effective when the chief satellite is in the circular orbit and the relative separation distance is small. On the other hand, the SDRE-based formulation is found to be effective even for eccentric orbits, but only with small eccentricity.
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Satellite Orbital Dynamics, the classic ., where two celestial bodies keep moving under the gravitational influence of each other. This chapter presents an overview of the two-body orbital mechanics first. Satellite orbital dynamics is presented next, which is a special case of the two-body problem, where the mass of one cele
发表于 2025-3-22 23:43:37 | 显示全部楼层
Infinite-Time LQR and SDRE for Satellite Formation Flying,n linear and nonlinear optimal controllers to achieve the objective of satellite formation flying. Infinite-time formulations of LQR and SDRE offer the advantage of simplicity naturally and hence they are widely preferred in various applications. The utility of these methods for satellite formation
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Adaptive Dynamic Inversion for Satellite Formation Flying,in elliptic orbits, etc. However, under the above-enhanced conditions, linear system dynamics based control design approaches fail to achieve the desired objectives. Even though the LQR philosophy inspired the SDRE approach discussed in Chapter . offers a limited solution, it suffers from the drawba
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