Orbital Mechanics, Third Edition

Chobotov, V. A.

doi:10.2514/4.862250

Cited by 131 publications

(133 citation statements)

References 12 publications

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“…This subject is arranged at the end of Chapter 5 in the author's book of Advanced Dynamics [2]. That means students have the basic knowledge in particle dynamics.…”

Section: Interplanetary Trajectoriesmentioning

confidence: 99%

Foundation of Graduate Study in Mechanical Engineering—Advanced Dynamics

Ying¹

2016

JEPE

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“…This subject is arranged at the end of Chapter 5 in the author's book of Advanced Dynamics [2]. That means students have the basic knowledge in particle dynamics.…”

Section: Interplanetary Trajectoriesmentioning

confidence: 99%

Foundation of Graduate Study in Mechanical Engineering—Advanced Dynamics

Ying¹

2016

JEPE

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“…When orbits are low-altitude ones, less than 1000 km, the drag effect should be considered in long-term predictions. The perturbing acceleration due to drag effect could be given as [1]:…”

Section: Perturbation Due To Atmospheric Dragmentioning

confidence: 99%

“…To include the effects of the perturbations, the equation of motion is written in a general form as [1]:…”

Section: Perturbations At Gps Satellite Orbitsmentioning

confidence: 99%

GPS as a base for analysis of perturbations of space based and ground based applications

Traykova

Radkov

2017

MATEC Web Conf.

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Abstract. The present work is dedicated to examining the impact of respective Navstar/GPS embarrass impact on the running of the global navigation system as well as synthesizing a computer program for their impact judgment as well. Two major groups of perturbation factors are addressed: perturbations proven impact on the orbital segment and perturbations proven impact on the running of the user's piston ring (nonorbital disturbances); it is being synthesized in the theoretical productions on the ground, plan code that yes on is modeled. The influence of those who embarrass the invoices on the accuracy of specifying the location.

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“…With these assumptions, Edelbaum derived the following set of equations for the lowthrust orbit transfer 57,58 : …”

Section: Preliminary Orbit Maneuvering Analysismentioning

confidence: 99%

The dynamics and control of the CubeSail mission: A solar sailing demonstration

Pukniel

Coverstone

Burton

et al. 2011

Advances in Space Research

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The proposed study addresses two issues related to the slow emergence of solar sailing as a viable space propulsion method. The low technology readiness level and complications related to stowage, deployment, and support of the sail structure are both addressed by combining the CU Aerospace and University of Illinois-developed UltraSail and CubeSat expertise to design a small-scale solar sail deployment and propulsion experiment in low Earth orbit. The study analyzes multiple aspects of the problem from initial sizing and packaging of the solar sail film into two CubeSat-class spacecraft, through on-orbit deployment dynamics, attitude control of large and flexible space structure, and predictions of performance and orbital maneuvering capability.iii ACKNOWLEDGEMENTS

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Orbital Mechanics, Third Edition

Cited by 131 publications

References 12 publications

Foundation of Graduate Study in Mechanical Engineering—Advanced Dynamics

Foundation of Graduate Study in Mechanical Engineering—Advanced Dynamics

GPS as a base for analysis of perturbations of space based and ground based applications

The dynamics and control of the CubeSail mission: A solar sailing demonstration

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