Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters (Hardcover, 1st ed. 2022)

This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.

General

Imprint:	Springer Verlag, Singapore
Country of origin:	Singapore
Release date:	September 2021
First published:	2022
Authors:	Jie Wang • Dong-Xu Li
Dimensions:	235 x 155mm (L x W)
Format:	Hardcover
Pages:	185
Edition:	1st ed. 2022
ISBN-13:	978-981-16-5096-3
Categories:	Books > Reference & Interdisciplinary > Communication studies > Information theory > Cybernetics & systems theory Books > Professional & Technical > Transport technology > Aerospace & aviation technology > General Books > Professional & Technical > Electronics & communications engineering > Electronics engineering > Automatic control engineering > General Promotions
LSN:	981-16-5096-9
Barcode:	9789811650963

Is the information for this product incomplete, wrong or inappropriate? Let us know about it.

Does this product have an incorrect or missing image? Send us a new image.

Is this product missing categories? Add more categories.

Review This Product

No reviews yet - be the first to create one!