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100   $a20181220d2019      u|             0
101 0 $aeng
135   $aurcnu||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOptimal Space Flight Navigation$b[electronic resource] $eAn Analytical Approach /$fby Ashish Tewari
205   $a1st ed. 2019.
210  1$aCham :$cSpringer International Publishing :$cImprint: Birkhäuser,$d2019.
215   $a1 online resource (277 pages)
225 1 $aControl Engineering,$x2373-7719
311   $a3-030-03788-6 
327   $a1. Introduction -- 2. Analytical Optimal Control -- 3. Orbital Mechanics and Impulsive Transfer -- 4. Two-Body Maneuvers with Unbounded Continuous Inputs -- 5. Optimal Maneuvers with Bounded Inputs -- 6. Flight in Non-spherical Gravity Fields.
330   $aThis book consolidates decades of knowledge on space flight navigation theory, which has thus far been spread across various research articles. By gathering this research into a single text, it will be more accessible to students curious about the study of space flight navigation. Books on optimal control theory and orbital mechanics have not adequately explored the field of space flight navigation theory until this point. The opening chapters introduce essential concepts within optimal control theory, such as the optimization of static systems, special boundary conditions, and dynamic equality constraints. An analytical approach is focused on throughout, as opposed to computational. The result is a book that emphasizes simplicity and practicability, which makes it accessible and engaging. This holds true in later chapters that involve orbital mechanics, two-body maneuvers, bounded inputs, and flight in non-spherical gravity fields. The intended audience is primarily upper-undergraduate students, graduate students, and researchers of aerospace, mechanical, and/or electrical engineering. It will be especially valuable to those with interests in spacecraft dynamics and control. Readers should be familiar with basic dynamics and modern control theory. Additionally, a knowledge of linear algebra, variational methods, and ordinary differential equations is recommended.
410  0$aControl Engineering,$x2373-7719
606   $aSystem theory
606   $aControl engineering
606   $aCalculus of variations
606   $aAerospace engineering
606   $aAstronautics
606   $aSystems Theory, Control$3https://scigraph.springernature.com/ontologies/product-market-codes/M13070
606   $aControl and Systems Theory$3https://scigraph.springernature.com/ontologies/product-market-codes/T19010
606   $aCalculus of Variations and Optimal Control; Optimization$3https://scigraph.springernature.com/ontologies/product-market-codes/M26016
606   $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050
615  0$aSystem theory.
615  0$aControl engineering.
615  0$aCalculus of variations.
615  0$aAerospace engineering.
615  0$aAstronautics.
615 14$aSystems Theory, Control.
615 24$aControl and Systems Theory.
615 24$aCalculus of Variations and Optimal Control; Optimization.
615 24$aAerospace Technology and Astronautics.
676   $a629.4742
700   $aTewari$b Ashish$4aut$4http://id.loc.gov/vocabulary/relators/aut$0755492
906   $aBOOK
912   $a9910337654603321
996   $aOptimal Space Flight Navigation$91945072
997   $aUNINA