Access the full text.
Sign up today, get DeepDyve free for 14 days.
Xiangyuan Zeng, Junfeng Li, H. Baoyin, Shengping Gong (2011)
Trajectory optimization and applications using high performance solar sailsTheoretical and Applied Mechanics Letters, 1
C. Sauer (1999)
Solar Sail Trajectories for Solar Polar and Interstellar Probe Missions
Xiangyuan Zeng, K. Alfriend, S. Vadali (2014)
Solar Sail Planar Multireversal Periodic OrbitsJournal of Guidance Control and Dynamics, 37
Xiangyuan Zeng, H. Baoyin, Junfeng Li, Shengping Gong (2011)
Three-dimensional time optimal double angular momentum reversal trajectory using solar sailsCelestial Mechanics and Dynamical Astronomy, 111
Xiangyuan Zeng, Shengping Gong, Junfeng Li, K. Alfriend (2016)
Solar Sail Body-Fixed Hovering over Elongated AsteroidsJournal of Guidance Control and Dynamics, 39
A. E. Roy (2005)
Orbital motionProceedings of the Institute of Physics Publishing
J. Calamia (2010)
Space sailingIEEE Spectrum, 47
M. Leipold, O. Wagner (1998)
'Solar Photonic Assist' Trajectory Design for Solar Sail Missions to the Outer Solar System and Beyond, 100
(2016)
Impact risk analysis of Near-Earth asteroids with multiple successive Earth encounters
A. Quarta, G. Mengali (2011)
Engineering Notes Solar Sail Capabilities to Reach Elliptic Rectilinear Orbits
Xiangyuan Zeng, K. Alfriend, Junfeng Li, S. Vadali (2012)
Optimal Solar Sail Trajectory Analysis for Interstellar MissionsThe Journal of the Astronautical Sciences, 59
G. Vulpetti (2011)
Reaching extra-solar-system targets via large post-perihelion lightness-jumping sailcraftActa Astronautica, 68
Gong Sheng-ping (2012)
A solar sail inverse periodic orbitJournal of Tsinghua University
G. Vulpetti (2001)
Sailcraft-based mission to the Solar Gravitational Lens, 504
(2001)
Sail flatness, attitude, and orbit control issues for an ST-7 solar sail spacecraft
B. Dachwald (2004)
Optimal Solar Sail Trajectories for Missions to the Outer Solar SystemJournal of Guidance Control and Dynamics, 28
I. Dandouras, B. Pirard, J. Prado (2004)
High performance solar sails for linear trajectories and heliostationary missionsAdvances in Space Research, 34
M. Macdonald, C. McInnes (2010)
Solar sail mission applications and future advancement
R. Broucke (1980)
Orbital motionCelestial mechanics, 21
G. Vulpetti (2012)
Fast Solar Sailing: Astrodynamics of Special Sailcraft Trajectories
Fanghua Jiang, H. Baoyin, Junfeng Li (2012)
Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic ApproachJournal of Guidance Control and Dynamics, 35
(2013)
Time-optimal trajectory design for a dualsatellite sailcraft interstellar mission with probe release (AAS 13–221)
M. Macdonald, C. McInnes, Gareth Hughes (2010)
Technology requirements of exploration beyond Neptune by solar sail propulsionJournal of Spacecraft and Rockets, 47
C. McInnes (1999)
Solar Sailing: Technology, Dynamics and Mission Applications
Xiangyuan Zeng, Shengping Gong, Junfeng Li (2014)
Earth-crossing asteroid intercept mission with a solar sail spacecraftIEEE Aerospace and Electronic Systems Magazine, 29
G. Colombo, D. Lautman, G. Pettengill (1976)
An Alternative Option to the Dual-Probe Out-of-Ecliptic Mission Via Jupiter Swingby
(1992)
Missions to the heliopause and beyond by staged propulsion spacecrafts
Binfeng Pan, P. Lu, Xun Pan, Yangyang Ma (2016)
Double-Homotopy Method for Solving Optimal Control ProblemsJournal of Guidance Control and Dynamics, 39
Xiangyuan Zeng, H. Baoyin, Junfeng Li, Shengping Gong (2011)
Feasibility analysis of the angular momentum reversal trajectory via hodograph method for high performance solar sailsScience China Technological Sciences, 54
Xiangyuan Zeng, H. Baoyin, Junfeng Li, Shengping Gong (2011)
New applications of the H-reversal trajectory using solar sailsResearch in Astronomy and Astrophysics, 11
T. Pino, C. Circi (2017)
A star-photon sailcraft mission in the Alpha Centauri systemAdvances in Space Research, 59
A. Quarta, G. Mengali (2013)
Optimal Solar Sail Transfer to Linear TrajectoriesActa Astronautica, 82
G. Mengali, A. A. Quarta, D. Romagnoli, C. Circi (2011)
H2-reversal trajectory: a new mission application for highperformance solar sailsAdvances in Space Research, 48
(2013)
Key technologies to enable nearterm interstellar scientific precursor missions
G. Vulpetti (1996)
3D high-speed escape heliocentric trajectories by all-metallic-sail low-mass sailcraftActa Astronautica, 39
Shengping Gong, Junfeng Li, Xiangyuan Zeng (2011)
Utilization of an H-reversal trajectory of a solar sail for asteroid deflectionResearch in Astronomy and Astrophysics, 11
G. Vulpetti (1997)
Sailcraft at high speed by orbital angular momentum reversalActa Astronautica, 40
G. Matloff, G. Vulpetti, C. Bangs, R. Haggerty, L. Johnson (2002)
The Interstellar Probe (ISP): Pre-Perihelion Trajectories and Application of Holography
A. Lyngvi, P. Falkner, A. Peacock (2005)
The interstellar heliopause probe technology reference studyAdvances in Space Research, 35
G. Vulpetti (1999)
General 3D H-reversal trajectories for high-speed sailcraftActa Astronautica, 44
Alan Pitz, B. Kaplinger, G. Vardaxis, Tim Winkler, B. Wie (2012)
Conceptual design of a hypervelocity asteroid intercept vehicle (HAIV) and its flight validation missionActa Astronautica, 94
L. Johnson, S. Leifer (2000)
Propulsion Options for Interstellar Exploration.
The set of the orbital angular-momentum reversal, or H-reversal, sailcraft trajectory was born as a type of unconventional precursor interstellar mission trajectory by using highperformance solar sails. Starting from an outline of the H-reversal sail trajectory, this paper mainly focuses on the 2D reversal-mode solution to the general solar-photon sail motion equations. The feasible region for H-reversal trajectories in fixed sail attitude angles is illustrated. Some interesting applications of the H-reversal trajectory are presented in detail to show its advantages. As a special case, a precursor interstellar probe can be delivered with a constant sail orientation in the H-reversal trajectory to be compared with the direct-motion sail flyby of the Sun. Of importance are the heliocentric periodic orbits in double H-reversal modes, obtained via both fixed and time-varying sail attitude angles. Two more applications involving H-reversal trajectories are discussed in terms of asteroid deflection and transfer trajectory to rectilinear orbits. Finally, some items of the mathematics behind the 3D motion-reversal trajectories are summarized.
Astrodynamics – Springer Journals
Published: Mar 1, 2019
Keywords: solar-photon sailing; sailcraft; lightness number; orbital H-reversal mode
Read and print from thousands of top scholarly journals.
Already have an account? Log in
Bookmark this article. You can see your Bookmarks on your DeepDyve Library.
To save an article, log in first, or sign up for a DeepDyve account if you don’t already have one.
Copy and paste the desired citation format or use the link below to download a file formatted for EndNote
Access the full text.
Sign up today, get DeepDyve free for 14 days.
All DeepDyve websites use cookies to improve your online experience. They were placed on your computer when you launched this website. You can change your cookie settings through your browser.