Navigation and Guidance of Orbital Transfer Vehicle
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Beschreibung
This book uses the entire flying process, starting from ground launching of the orbital transfer vehicle (OTV) to injecting payload into earth synchronous orbit, as an example for real-world engineering practices. It discusses in detail the analysis design and integrated OTV navigation and guidance system technologies in combination with the engineering experiences of the authors in analysis, design and integrated OTV navigation and guidance system applications, and the research on navigation and guidance theories. It focuses on establishing motion of air vehicle equations, control system hardware components, orbit prediction technology, inertial navigation and initial alignment technologies, INS/GNSS integrated navigation technologies, INS/CNS integrated navigation technologies, redundant fault tolerance and failure reconfiguration technology of inertial sensors, guidance and midcourse correction technologies and orbit control strategies.
The book is a valuablereference book for the engineers, technicians and researchers who are engaged in analysis, design and integrated application of OTV navigation and guidance control systems. It can also be used as teaching material for postgraduates and senior undergraduates majoring in OTV navigation and guidance systems and other related subjects.
Uses the entire flying process, starting from ground launching of orbital transfer vehicle (OTV) to injecting payload into earth synchronous orbit, as an example for real-world engineering practices
Organized in a coherent style making it easy to understand
Divides the vary-trajectory control of space vehicles into the guidance realized by the sustainer motor and the midcourse correction fulfilled by the small engine, pertinent to the actual OTV flight features
Uses the entire flying process, starting from ground launching of orbital transfer vehicle (OTV) to injecting payload into earth synchronous orbit, as an example for real-world engineering practices Organized in a coherent style making it easy to understand Divides the vary-trajectory control of space vehicles into the guidance realized by the sustainer motor and the midcourse correction fulfilled by the small engine, pertinent to the actual OTV flight features Includes supplementary material: sn.pub/extras
Autor*in
Xuefeng Li
Themen in »Navigation and Guidance of Orbital Transfer Vehicle«
Orbital Transfer Vehicle system OTV launch Space navigation Control system Orbit prediction Motional equation Inertial navigation Initial alignment Navigation technology Orbit control Orbital Transfer Vehicle