Optimal Reusable Rocket Landing Guidance: A Cutting-Edge Approach Integrating Scientific Machine Learning and Enhanced Neural Networks
Author:
Affiliation:
1. Centre for Cyberphysical and Autonomous Systems, Cranfield University, Bedford, U.K.
2. Data Products Department, UDemy Inc., San Francisco, CA, USA
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/6287639/10380310/10415408.pdf?arnumber=10415408
Reference50 articles.
1. Successive Convexification for Fuel-Optimal Powered Landing with Aerodynamic Drag and Non-Convex Constraints
2. Design of the landing guidance for the retro-propulsive vertical landing of a reusable rocket stage
3. Integrated Optimal Guidance for Reentry and Landing of a Rocket Using Multi-Phase Pseudo-Spectral Convex Optimization
4. Survey of autonomous guidance methods for powered planetary landing
5. A guidance and control assessment of three vertical landing options for RLV
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1. Powered Descent Guidance via First-Order Optimization With Expansive Projection;IEEE Access;2024
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