Abstract

The abort mission refers to the mission where the landing vehicle needs to terminate the landing mission when an anomaly happens and be safely guided to the desired orbit. This paper focuses on solving the time-optimal abort guidance (TOAG) problem in real-time via the feature-based learning method. First, according to the optimal control theory, the features are identified to represent the optimal solutions of TOAG using a few parameters. After that, a sufficiently large data set of time-optimal abort trajectories is generated offline by solving the TOAG problems with different initial conditions. Then, the features are extracted for all generated cases. To find the implicit relationships between the initial conditions and identified features, neural networks are constructed to map the relationships based on the generated data set. Finally, experimental flight tests are conducted to demonstrate the onboard computation capability and effectiveness of the proposed method.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 2March 2024

History

Received: Dec 27, 2022
Accepted: Oct 17, 2023
Published online: Dec 30, 2023
Published in print: Mar 1, 2024
Discussion open until: May 30, 2024

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Vinay Kenny [email protected]
Graduate Research Associate, School of Aeronautics and Astronautics, Purdue Univ., 701 W. Stadium Ave., West Lafayette, IN 47907. Email: [email protected]
Graduate Research Associate, School of Aeronautics and Astronautics, Purdue Univ., 701 W. Stadium Ave., West Lafayette, IN 47907. ORCID: https://orcid.org/0000-0002-4729-6422. Email: [email protected]
Chaoying Pei [email protected]
Graduate Research Associate, School of Aeronautics and Astronautics, Purdue Univ., 701 W. Stadium Ave., West Lafayette, IN 47907. Email: [email protected]
Godfrey Hendrix [email protected]
Graduate Research Associate, School of Aeronautics and Astronautics, Purdue Univ., 701 W. Stadium Ave., West Lafayette, IN 47907. Email: [email protected]
Graduate Research Associate, School of Aeronautics and Astronautics, Purdue Univ., 701 W. Stadium Ave., West Lafayette, IN 47907. Email: [email protected]
Associate Professor, School of Aeronautics and Astronautics, Purdue Univ., 701 W. Stadium Ave., West Lafayette, IN 47907 (corresponding author). ORCID: https://orcid.org/0000-0001-6791-2512. Email: [email protected]
Jeremy Rea
System Manager, Flight Mechanics and Trajectory Design Branch, 2101 NASA Pkwy, Houston, TX 77058.

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