Pterodactyl: Guidance and Control of a Symmetric Deployable Entry Vehicle using an Aerodynamic Control System
Author:
Affiliation:
1. NASA Ames Research Center
2. NASA Johnson Space Center
Publisher
American Institute of Aeronautics and Astronautics
Reference25 articles.
1. Adaptive Deployable Entry and Placement Technology (ADEPT): A Feasibility Study for Human Missions to Mars
2. Survey of planetary entry guidance algorithms
3. Pterodactyl: Trade Study for an Integrated Control System Design of a Mechanically Deployed Entry Vehicle
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2. Optimal Mars Entry Trajectories for Bank-Angle and Alpha-Beta Steering;2024 IEEE Aerospace Conference;2024-03-02
3. Assessment of Control Algorithms for Mars Entry Vehicles with Flap-Based Trajectory Control;AIAA SCITECH 2024 Forum;2024-01-04
4. SimuPy Flight Vehicle Toolkit;Journal of Open Source Software;2022-07-07
5. Control of a Blunt Body Mars Entry Vehicle with Flaps Using Model Predictive Control;AIAA SCITECH 2022 Forum;2022-01-03
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