Solar sail trajectory analysis with asymptotic expansion method-Reference-Cited by-同舟云学术

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Solar sail trajectory analysis with asymptotic expansion method

Published:2017-09 Issue: Volume:68 Page:431-440
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Niccolai Lorenzo,Quarta Alessandro A.^ORCID,Mengali Giovanni^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Achievement of IKAROS – Japanese deep space solar sail demonstration mission;Tsuda,2011

2. Attitude control of IKAROS solar sail spacecraft and its flight results;Mori,2010

3. Fuel-free and oscillation-free attitude control of IKAROS solar sail spacecraft using reflectivity control device;Funase,2011

4. NanoSail-D: a solar sail demonstration mission;Johnson;Acta Astronaut.,2011

5. Near-earth asteroid (NEA) scout;McNutt,2014

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1. Optimal multi-segment trajectory of solar sail with analytical approximation;Aerospace Science and Technology;2024-10

2. Analytical Trajectory of Solar Sail With Fixed Pitch Angle From Elliptical Orbits;IEEE Transactions on Aerospace and Electronic Systems;2024-06

3. Fast Analysis of Multi-Asteroid Exploration Mission Using Multiple Electric Sails;Journal of Guidance, Control, and Dynamics;2023-05

4. Trajectory Analysis of a Zero-Pitch-Angle E-Sail with Homotopy Perturbation Technique;Journal of Guidance, Control, and Dynamics;2023-04

5. Application of homotopy perturbation method to the radial thrust problem;Astrodynamics;2022-11-23

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