Spacecraft dynamics and control : the embedded model control approach

Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform and systematic way of approaching space engineering control problems from the standpoint of model-based control, using state-space equations as the key paradigm for simulation, design and implementation. The book...

Full description

Saved in:
Bibliographic Details
Main Authors: Canuto, Enrico, (Author), Novara, Carlo, (Author), Massotti, Luca, (Author), Carlucci, Donato, (Author), Montenegro, Carlos Perez, (Author)
Format: eBook
Language: English
Published: Cambridge, MA : Butterworth-Heinemann, [2018]
Series: Aerospace engineering
Subjects:
Space vehicles > Dynamics.
Space vehicles > Control systems.
elektronické knihy
electronic books
ISBN: 9780081017951
0081017952
9780081007006
0081007000
Physical Description: 1 online resource

Cover

Table of contents

LEADER 04318cam a2200445 i 4500
001 kn-on1028553070
003 OCoLC
005 20240717213016.0
006 m o d
007 cr cn|||||||||
008 180313s2018 mau ob 001 0 eng d
040 |a N$T  |b eng  |e rda  |e pn  |c N$T  |d N$T  |d YDX  |d NLE  |d COO  |d OPELS  |d OCLCF  |d STF  |d MERER  |d D6H  |d QCL  |d OCLCQ  |d UAB  |d SNM  |d UPM  |d OCLCQ  |d U3W  |d LVT  |d KNOVL  |d CEF  |d VLB  |d UKAHL  |d UKMGB  |d S2H  |d OCLCO  |d OCLCQ  |d OCLCO  |d K6U  |d OCLCQ  |d SFB  |d OCLCQ  |d OCLCO  |d OCLCL  |d SXB  |d OCLCQ  |d OCLCO 
020 |a 9780081017951  |q (electronic bk.) 
020 |a 0081017952  |q (electronic bk.) 
020 |z 9780081007006 
020 |z 0081007000 
035 |a (OCoLC)1028553070  |z (OCoLC)1028781302  |z (OCoLC)1028891143  |z (OCoLC)1028949262  |z (OCoLC)1028971234  |z (OCoLC)1029005548  |z (OCoLC)1029209361 
100 1 |a Canuto, Enrico,  |e author. 
245 1 0 |a Spacecraft dynamics and control :  |b the embedded model control approach /  |c Enrico Canuto, Carlo Novara, Luca Massotti, Donato Carlucci, Carlos Perez Montenegro. 
264 1 |a Cambridge, MA :  |b Butterworth-Heinemann,  |c [2018] 
300 |a 1 online resource 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 0 |a Aerospace engineering 
504 |a Includes bibliographical references and index. 
505 0 |a 1. Introduction; 2. Attitude Representation; 3. Orbital Dynamics; 4. The Environment: Perturbing Forces and Torques; 5. Perturbed Orbital Dynamics; 6. Attitude Kinematics: Modeling and Feedback; 7. Attitude Dynamics: Modeling and Control; 8. Orbit and Attitude Sensors; 9. Orbit and Attitude Actuators; 10. Attitude Determination; 11. Orbital Control and Prediction Problems; 12. Attitude Control: A Case Study; 13. Introduction to Dynamic Systems; 14. Introduction to Embedded Model Control; Index. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |a Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform and systematic way of approaching space engineering control problems from the standpoint of model-based control, using state-space equations as the key paradigm for simulation, design and implementation. The book introduces the Embedded Model Control methodology for the design and implementation of attitude and orbit control systems. The logic architecture is organized around the embedded model of the spacecraft and its surrounding environment. The model is compelled to include disturbance dynamics as a repository of the uncertainty that the control law must reject to meet attitude and orbit requirements within the uncertainty class. The source of the real-time uncertainty estimation/prediction is the model error signal, as it encodes the residual discrepancies between spacecraft measurements and model output. The embedded model and the uncertainty estimation feedback (noise estimator in the book) constitute the state predictor feeding the control law. Asymptotic pole placement (exploiting the asymptotes of closed-loop transfer functions) is the way to design and tune feedback loops around the embedded model (state predictor, control law, reference generator). The design versus the uncertainty class is driven by analytic stability and performance inequalities. The method is applied to several attitude and orbit control problems. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Space vehicles  |x Dynamics. 
650 0 |a Space vehicles  |x Control systems. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Novara, Carlo,  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PCjFkFG4FfBJFjHpMRgwKkC 
700 1 |a Massotti, Luca,  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PCjy3D7K63Pjq64PvKFQJtC 
700 1 |a Carlucci, Donato,  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PCjt9q8QBpgTxywkyrjjX3P 
700 1 |a Montenegro, Carlos Perez,  |e author.  |1 https://id.oclc.org/worldcat/entity/E39PCjFvRcpy8BpxRTDyCKww83 
776 0 8 |i Print version:  |z 9780081007006  |z 0081007000  |w (OCoLC)992433770 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpSDCTEMC5/spacecraft-dynamics-and?kpromoter=marc  |y Full text 

Similar Items