Integrated Guidance and Control for Strap-Down Flight Vehicle: A Deep Reinforcement Learning Approach
This paper proposes a three-dimensional (3D) deep reinforcement learning-based integrated guidance and control (DRLIGC) method, which is restricted by the narrow field-of-view (FOV) constraint of the strap-down seeker. By leveraging the data-driven nature of the deep reinforcement learning (DRL) algorithm, this method mitigates the challenges associated with integrated guidance and control (IGC) method design arising from model dependencies, thereby addressing the inherent complexity of the IGC model. Firstly, according to different states and actions, the pitch and yaw channels of the six-degree-of-freedom (6-DOF) IGC model are modeled as Markov decision processes (MDPs). Secondly, a channel-by-channel progressive training method based on the twin delayed deep deterministic policy gradient (TD3) algorithm is proposed. The agents of the pitch and yaw channels are trained using the TD3 algorithm independently, which substantially alleviates the complexity of the training process, while the roll channel is stabilized through the application of the back-stepping method. Thirdly, a comprehensive reward function is designed to simultaneously address the narrow FOV constraint and enhance the target engagement capability. Additionally, this function mitigates the issue of sparse rewards to some extent. Through Monte Carlo (MC) and comparative simulation verification, it is shown that the DRLIGC method proposed in this paper can effectively approach the target while maintaining the narrow FOV constraint and also has good robustness.
Authors
- Jiale Zhang (ORCID: https://orcid.org/0000-0002-4012-7677)
- Qinglong Zhang (ORCID: https://orcid.org/0000-0002-4006-2164)
- Jingyan Zhang (ORCID: https://orcid.org/0000-0003-4492-1584)
- Bin Zhao (ORCID: https://orcid.org/0000-0002-8731-2503)
- Yifu Jiang (ORCID: https://orcid.org/0000-0003-3044-8060)
Institutions
- Northwestern Polytechnical University (CN)
Publication Details
- Journal
- Aerospace
- Published
- 2025-05-01
- DOI
- https://doi.org/10.3390/aerospace12050400
- Primary Topic
- Guidance and Control Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.00
Funders
- National Natural Science Foundation of China