Design and Flight Testing of a Rocket-Launched Folding UAV for Earth and Planetary Exploration Applications
Author:
Affiliation:
1. Queensland University of Technology,Brisbane City,QLD,Australia,4000
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9843190/9843194/09843481.pdf?arnumber=9843481
Reference21 articles.
1. Confined spaces industrial inspection with micro aerial vehicles and laser range finder localization
2. Dynamic analysis of wing deployment of high altitude balloon launched small size folding-wing UAV
3. Design of a Ballistically-Launched Foldable Multirotor
4. Design and Autonomous Stabilization of a Ballistically-Launched Multirotor
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1. Compact and Lightweight Foldable Umbrella Heatshield for CanSat-Scale Planetary Probes Lander Mission;2024 International Electronics Symposium (IES);2024-08-06
2. Design of a Foldable Multirotor for Rapid Deployment in Complex Environments;Lecture Notes in Electrical Engineering;2024
3. Adjustable Fully Adaptive Cross-Entropy Algorithms for Task Assignment of Multi-UAVs;Drones;2023-03-16
4. Design and Implementation of a Low-Cost Folding-Wing UAV for Model Rocket Deployment;2023 IEEE Aerospace Conference;2023-03-04
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