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Simplified technique for determining pericynthion altitude of lunar orbits
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Year: 1968 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Two-burn escape maneuvers with an intermediate coasting ellipse
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Year: 1969 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Applied nonsingular astrodynamics : optimal low-thrust orbit transfer
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ISBN: 1108576753 1108611087 Year: 2018 Publisher: Cambridge, England : Cambridge University Press,

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This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research students in aerospace engineering, as well as practitioners in the field of spaceflight dynamics, in developing simulation software to carry out trade studies useful in vehicle and mission design. It will teach readers to develop flight software for operational applications in autonomous mode, so to actually transfer space vehicles from one orbit to another. The practical, real-life applications discussed will give readers a clear understanding of the mathematics of orbit transfer, allow them to develop their own operational software to fly missions, and to use the contents as a research tool to carry out even more complex analyses.


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Spacecraft Manoeuvring in the Vicinity of a near-Circular Orbit.
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ISBN: 9781527584730 1527584739 Year: 2022 Publisher: Newcastle-upon-Tyne

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This book sets forth the theory of optimal manoeuvring in the vicinity of a circular orbit, describing the possible types of optimal solutions for the transfer and rendezvous problems in cases of coplanar and non-coplanar orbits. In order to find the manoeuvre parameters of these solutions, the book presents extremely simple analytical and numerical-analytical methods, and shows how they can be applied for the solution of basic manoeuvre problems for real spacecraft. It also details effective methods, used both in Russia and across the globe, for the active space object manoeuvre assessment, which will help to propagate collision hazards more accurately.


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Effect of departure delays on manned Mars mission selection
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Year: 1995 Publisher: Washington, DC : American Institute of Aeronautics and Astronautics,

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Applied nonsingular astrodynamics optimal low-thrust orbit transfer
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ISBN: 9781108472364 9781108560061 Year: 2018 Publisher: Cambridge Cambridge University Press

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This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research students in aerospace engineering, as well as practitioners in the field of spaceflight dynamics, in developing simulation software to carry out trade studies useful in vehicle and mission design. It will teach readers to develop flight software for operational applications in autonomous mode, so to actually transfer space vehicles from one orbit to another. The practical, real-life applications discussed will give readers a clear understanding of the mathematics of orbit transfer, allow them to develop their own operational software to fly missions, and to use the contents as a research tool to carry out even more complex analyses. [Publisher]


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Fly me to the moon : an insider's guide to the new science of space travel
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ISBN: 1400849195 9781400849192 Year: 2007 Publisher: Princeton : Princeton University Press,

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When a leaf falls on a windy day, it drifts and tumbles, tossed every which way on the breeze. This is chaos in action. In Fly Me to the Moon, Edward Belbruno shows how to harness the same principle for low-fuel space travel--or, as he puts it, "surfing the gravitational field." Belbruno devised one of the most exciting concepts now being used in space flight, that of swinging through the cosmos on the subtle fluctuations of the planets' gravitational pulls. His idea was met with skepticism until 1991, when he used it to get a stray Japanese satellite back on course to the Moon. The successful rescue represented the first application of chaos to space travel and ushered in an emerging new field. Part memoir, part scientific adventure story, Fly Me to the Moon gives a gripping insider's account of that mission and of Belbruno's personal struggles with the science establishment. Along the way, Belbruno introduces readers to recent breathtaking advances in American space exploration. He discusses ways to capture and redirect asteroids; presents new research on the origin of the Moon; weighs in on discoveries like 2003 UB313 (now named Eris), a dwarf planet detected in the far outer reaches of our solar system--and much more. Grounded in Belbruno's own rigorous theoretical research but written for a general audience, Fly Me to the Moon is for anybody who has ever felt moved by the spirit of discovery.


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Orbital relative motion and terminal rendezvous : analytic and numerical methods for spaceflight guidance applications
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ISBN: 3030646572 3030646564 Year: 2021 Publisher: Cham, Switzerland : Springer,


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Navigation and Guidance of Orbital Transfer Vehicle
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ISBN: 9811063346 9811063338 Year: 2018 Publisher: Singapore : Springer Singapore : Imprint: Springer,

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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 valuable reference 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.

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