Spacecraft Dynamics and Control: An Introduction [Bookshelf]


This book consists of twenty six chapters and two appendices. The exposition is divided into roughly 5 components: Basic kinematics and dynamics of particles and rigid bodies; Orbital mechanics of purpose mass objects; Spacecraft angle dynamics; Feedback management theory; and Pactical applications of the above four to spacecraft management. This book can be considered as a prequel to those wishing to review the additional advanced graduate-level text of Hughes. Overall, I consider this book an wonderful pedagogical exposition of spacecraft dynamics and management, valuable for a student or skilled who has never before been exposed to the present material and needs to come back up to hurry with the basics of orbital mechanics, attitude kinematics and dynamics, and feedback control theory. A terribly notable feature of this book lies in the successful unifying treatment of spacecraft orbital dynamics, angle dynamics, and management using the vectrix calculus. For these reasons, I not solely strongly suggest this book for college students and practitioners, as well as educational and company libraries, however additionally have little doubt that this book can earn its place amongst the opposite glorious treatments of the topic mentioned above.

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PROJECT TITLE :Unified saturated proportional derivative control framework for asymptotic stabilisation of spacecraftABSTRACT:In this study, the authors propose a unified approach to saturated proportional spinoff (SPD) controller
PROJECT TITLE :Variations in Cathodoluminescent Intensity of Spacecraft Materials Exposed to Energetic Electron BombardmentABSTRACT:Several contemporary spacecraft materials exhibit cathodoluminescence when exposed to electron
PROJECT TITLE :Distributed finite-time attitude dynamic tracking control for multiple rigid spacecraftABSTRACT:During this study, the authors study the distributed finite-time perspective dynamic tracking control downside for
PROJECT TITLE :6-DOF integrated adaptive backstepping control for spacecraft proximity operationsABSTRACT:Relative motion management with half dozen degrees of freedom (vi DOF) is investigated for a chaser spacecraft with parametric
PROJECT TITLE :Medium-frequency disturbance attenuation for the spacecraft via virtual-gimbal tilting of the magnetically suspended reaction wheelABSTRACT:A medium-frequency disturbance attenuation strategy based on the virtual-gimbal

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