TY - GEN
T1 - Multi-step trajectory prediction method for Mars UAV based on Bidirectional Gated Recurrent Unit
AU - Zhu, Fu
AU - Zhu, Zhanxia
AU - Sun, Chong
AU - Wu, Yitong
N1 - Publisher Copyright:
Copyright © 2025 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2025
Y1 - 2025
N2 - As Mars exploration advances and mission complexity increases, the collaborative operation of multiple Mars Unmanned Aerial Vehicles (UAVs) can significantly enhance the efficiency of Mars exploration and data acquisition. However, the harsh Martian environment poses substantial challenges to UAV flight technology. Atmospheric disturbances such as wind speeds and sandstorms may significantly affect UAV trajectory, leading to deviations from the planned path and increasing the risk of collisions. Therefore, accurate UAV trajectory prediction is essential for real-time flight path adjustments and collision avoidance. This paper proposes a multi-step trajectory prediction method for Mars UAV, leveraging historical flight data to forecast future trajectories. Existing multi-step trajectory prediction approaches for UAV predominantly rely on single-step prediction, where each predicted track point is sequentially appended to historical trajectory data. The model's input is then iteratively updated using a sliding window mechanism to extend the prediction horizon. However, conventional methods suffer from error accumulation, where prediction errors at each step propagate through subsequent iterations, leading to a rapid decline in precision over time. To address this challenge, this paper proposes a multi-step trajectory prediction approach for UAV based on Bidirectional Gated Recurrent Unit (Bi-GRU) network. By leveraging a network model, the proposed method extracts essential features from the input sequence and directly predicts the full trajectory in a single forward pass, eliminating iterative updates and effectively mitigating error propagation. First, a UAV dynamics model is developed within simulation platform, incorporating Martian environmental parameters to generate reliable flight data. The UAV's position, attitude angles, and velocity are selected as key features to construct a comprehensive dataset. Subsequently, a neural network model is designed as the prediction framework, then the position, attitude, and velocity as input of network. Leveraging the bidirectional propagation mechanism of the Bi-GRU network, the model effectively captures temporal dependencies in both forward and reverse directions, enabling high-precision trajectory prediction. Next, historical trajectory parameters are utilized as input during model training to generate multi-step trajectory predictions. Finally, the prediction accuracy is evaluated using a validation dataset by comparing the predicted and actual trajectories. The results demonstrate that the proposed method outperforms conventional approaches, including LSTM and GRU, by achieving the lowest prediction error at the same step length. This validates its effectiveness in meeting the requirements for high-precision multi-step trajectory prediction.
AB - As Mars exploration advances and mission complexity increases, the collaborative operation of multiple Mars Unmanned Aerial Vehicles (UAVs) can significantly enhance the efficiency of Mars exploration and data acquisition. However, the harsh Martian environment poses substantial challenges to UAV flight technology. Atmospheric disturbances such as wind speeds and sandstorms may significantly affect UAV trajectory, leading to deviations from the planned path and increasing the risk of collisions. Therefore, accurate UAV trajectory prediction is essential for real-time flight path adjustments and collision avoidance. This paper proposes a multi-step trajectory prediction method for Mars UAV, leveraging historical flight data to forecast future trajectories. Existing multi-step trajectory prediction approaches for UAV predominantly rely on single-step prediction, where each predicted track point is sequentially appended to historical trajectory data. The model's input is then iteratively updated using a sliding window mechanism to extend the prediction horizon. However, conventional methods suffer from error accumulation, where prediction errors at each step propagate through subsequent iterations, leading to a rapid decline in precision over time. To address this challenge, this paper proposes a multi-step trajectory prediction approach for UAV based on Bidirectional Gated Recurrent Unit (Bi-GRU) network. By leveraging a network model, the proposed method extracts essential features from the input sequence and directly predicts the full trajectory in a single forward pass, eliminating iterative updates and effectively mitigating error propagation. First, a UAV dynamics model is developed within simulation platform, incorporating Martian environmental parameters to generate reliable flight data. The UAV's position, attitude angles, and velocity are selected as key features to construct a comprehensive dataset. Subsequently, a neural network model is designed as the prediction framework, then the position, attitude, and velocity as input of network. Leveraging the bidirectional propagation mechanism of the Bi-GRU network, the model effectively captures temporal dependencies in both forward and reverse directions, enabling high-precision trajectory prediction. Next, historical trajectory parameters are utilized as input during model training to generate multi-step trajectory predictions. Finally, the prediction accuracy is evaluated using a validation dataset by comparing the predicted and actual trajectories. The results demonstrate that the proposed method outperforms conventional approaches, including LSTM and GRU, by achieving the lowest prediction error at the same step length. This validates its effectiveness in meeting the requirements for high-precision multi-step trajectory prediction.
KW - Bi-GRU
KW - Mars UAV
KW - Trajectory prediction
UR - https://www.scopus.com/pages/publications/105040812902
U2 - 10.52202/083076-0116
DO - 10.52202/083076-0116
M3 - 会议稿件
AN - SCOPUS:105040812902
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 1071
EP - 1076
BT - IAF Space Exploration Symposium - Held at the 76th International Astronautical Congress, IAC 2025
PB - International Astronautical Federation, IAF
T2 - 2025 IAF Space Exploration Symposium at the 76th International Astronautical Congress, IAC 2025
Y2 - 29 September 2025 through 3 October 2025
ER -