Atjaunināt sīkdatņu piekrišanu

E-grāmata: Autonomous Trajectory Planning and Guidance Control for Launch Vehicles

Edited by , Edited by , Edited by
  • Formāts - EPUB+DRM
  • Cena: 3,93 €*
  • * ši ir gala cena, t.i., netiek piemērotas nekādas papildus atlaides
  • Ielikt grozā
  • Pievienot vēlmju sarakstam
  • Šī e-grāmata paredzēta tikai personīgai lietošanai. E-grāmatas nav iespējams atgriezt un nauda par iegādātajām e-grāmatām netiek atmaksāta.

DRM restrictions

  • Kopēšana (kopēt/ievietot):

    nav atļauts

  • Drukāšana:

    nav atļauts

  • Lietošana:

    Digitālo tiesību pārvaldība (Digital Rights Management (DRM))
    Izdevējs ir piegādājis šo grāmatu šifrētā veidā, kas nozīmē, ka jums ir jāinstalē bezmaksas programmatūra, lai to atbloķētu un lasītu. Lai lasītu šo e-grāmatu, jums ir jāizveido Adobe ID. Vairāk informācijas šeit. E-grāmatu var lasīt un lejupielādēt līdz 6 ierīcēm (vienam lietotājam ar vienu un to pašu Adobe ID).

    Nepieciešamā programmatūra
    Lai lasītu šo e-grāmatu mobilajā ierīcē (tālrunī vai planšetdatorā), jums būs jāinstalē šī bezmaksas lietotne: PocketBook Reader (iOS / Android)

    Lai lejupielādētu un lasītu šo e-grāmatu datorā vai Mac datorā, jums ir nepieciešamid Adobe Digital Editions (šī ir bezmaksas lietotne, kas īpaši izstrādāta e-grāmatām. Tā nav tas pats, kas Adobe Reader, kas, iespējams, jau ir jūsu datorā.)

    Jūs nevarat lasīt šo e-grāmatu, izmantojot Amazon Kindle.

This open access book highlights the autonomous and intelligent flight control of future launch vehicles for improving flight autonomy to plan ascent and descent trajectories onboard, and autonomously handle unexpected events or failures during the flight.





 





Since the beginning of the twenty-first century, space launch activities worldwide have grown vigorously. Meanwhile, commercial launches also account for the booming trend. Unfortunately, the risk of space launches still exists and is gradually increasing in line with the rapidly rising launch activities and commercial rockets. In the history of space launches, propulsion and control systems are the two main contributors to launch failures. With the development of information technologies, the increase of the functional density of hardware products, the application of redundant or fault-tolerant solutions, and the improvement of the testability of avionics, the launch losses caused by control systems exhibita downward trend, and the failures induced by propulsion systems become the focus of attention. Under these failures, the autonomous planning and guidance control may save the missions.





 





This book focuses on the latest progress of relevant projects and academic studies of autonomous guidance, especially on some advanced methods which can be potentially real-time implemented in the future control system of launch vehicles. In Chapter 1, the prospect and technical challenges are summarized by reviewing the development of launch vehicles.  Chapters 2 to 4 mainly focus on the flight in the ascent phase, in which the autonomous guidance is mainly reflected in the online planning. Chapters 5 and 6 mainly discuss the powered descent guidance technologies. Finally, since aerodynamic uncertainties exert a significant impact on the performance of the ascent / landing guidance control systems, the estimation of aerodynamic parameters, which are helpful to improve flight autonomy, is discussed in Chapter 7.





 





The book serves as a valuable reference for researchers and engineers working on launch vehicles. It is also a timely source of information for graduate students interested in the subject. 





 
1. Review, Prospect and Technical Challenge of Launch Vehicle.-
2. Autonomous Guidance Control for Ascent Flight.-
3. Ascent Predictive
Guidance for Thrust Drop Fault of Launch Vehicles Using Improved GS-MPSP.-
4. Birkho pseudospectral method and convex programming for trajectory
optimization.- 5.  Autonomous Descent Guidance via Sequential
Pseudospectral Convex Programming.
Zhengyu Song





Dr. Zhengyu Song is a research fellow of China Academy of Launch Vehicle Technology. He is also an adjunct professor of the College of Control Science and Engineering, Zhejiang University, China. In 2016, he was elected an academician of the International Academy of Astronautics. He is currently the chief designer of China's Long March-8 Launch Vehicle. His research interests include autonomous and intelligent flight system design of launch vehicles.





 





Dangjun Zhao





Dangjun Zhao is currently a professor in the School of Automation, Central South University, China.  He received his Ph.D. in control science and engineering from Huazhong University of Science and Technology, Wuhan, China, in 2011. His research interests include intelligent perception, optimal control of spacecrafts, and unmanned system.





 





Stephan Theil





Dr. Stephan Theil is the head of GNC Systems department at DLR's Instituteof Space Systems. He is a recognized expert in the field of spacecraft guidance, navigation, and control (GNC) and has been conducting research in spacecraft GNC for more than 25 years. He has led and worked on many projects in the areas of technologies for optical navigation of landing probes on moons, Mars, and asteroids; hybrid navigation for space transportation applications; and guidance and control for entry, descent and landing.





He has also authored and contributed to 140 publications in different fields of spacecraft GNC. As a recognized expert, he was appointed as a co-chair and chair of the Technical Committee on GNC of the Council of European Aerospace Societies (CEAS) from 2011 to 2019, a field editor for GNC of the CEAS Space Journal as well as technical committee member for the CEAS Specialist Conference on Guidance, Navigation & Control and the International ESA Conference on Guidance and Navigation Control Systems.





Additionally, Dr. Theil has taught several courses on space flight mechanics and GNC at the University of Bremen since 2001. He has supervised more than 60 Masters and 15 Ph.D. students.