Mission design for deep space 1: A low-thrust technology validation mission-Reference-Cited by-同舟云学术

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Mission design for deep space 1: A low-thrust technology validation mission

Published:1999-08 Issue:4-9 Volume:45 Page:381-388
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Rayman Marc D.,Chadbourne Pamela A.,Culwell Jeffery S.,Williams Steven N.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference3 articles.

1. Deep Space One: NASA's First Deep-Space Technology Validation Mission;Rayman Marc,1997

2. Optimization of Multiple Target Electric Propulsion Trajectories;Sauer,1973

3. Design of High-Accuracy Multiple Flyby Trajectories Using Constrained Optimization;Byrnes,1995

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1. Optimization, guidance, and control of low-thrust transfers from the Lunar Gateway to low lunar orbit;Acta Astronautica;2024-09

2. Constant-Thrust Orbital Transfer About Binary Asteroids Using Bilinear Tangent Guidance;IEEE Transactions on Aerospace and Electronic Systems;2024-08

3. Multiphase Homotopic Approaches for Best Solution to Low-Thrust Geocentric Trajectories;IEEE Transactions on Aerospace and Electronic Systems;2024-08

4. High Specific-Impulse Electrospray Explorer Trajectory Guidance and Control Air Bearing Demonstration;Journal of Spacecraft and Rockets;2024-05-28

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