Landing Gear Design, Fabrication, and Testing for the Ingenuity Mars Helicopter-Reference-Cited by-同舟云学术

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Landing Gear Design, Fabrication, and Testing for the Ingenuity Mars Helicopter

Published:2022-03-05 Issue: Volume: Page:
ISSN:
Container-title:2022 IEEE Aerospace Conference (AERO)
language:
Short-container-title:

Author:

Langberg Sara A.¹,Tyler Jeremy D.¹,Pipenberg Benjamin T.¹,Keennon Matthew T.¹,Zwaan Peter¹

Affiliation:

1. AeroVironment, Inc.,Simi Valley,CA,93065

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9843190/9843194/09843527.pdf?arnumber=9843527

Reference8 articles.

1. Guidance and Control for a Mars Helicopter

2. Flight control system for NASA's Mars Helicopter;grip;AIAA Science and Technology Forum,2018

3. Characterization of Mars Rover 2020 prospective landing sites leading up to the second downselection: (expanded abstract);golombek;48th Lunar and Planetary Science Abstract 2333,2017

4. Development of the Mars Helicopter Rotor System;pipenberg;Vertical Flight Society 75th Annual Forum & Technology Display,2019

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Slopes on Titan and application to spacecraft landing safety;Planetary and Space Science;2023-10

2. Analytic rock abundance distributions and their application to spacecraft landing hazards;Planetary and Space Science;2023-09

3. Sample Recovery Helicopter;2023 IEEE Aerospace Conference;2023-03-04

4. Conceptual Design of a Mars Rotorcraft for Future Sample Fetch Missions;2022 IEEE Aerospace Conference (AERO);2022-03-05

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