Research on the Design and Simulation of Missile Intelligent Agent Autopilot Integrated With Deep Reinforcement Learning

This paper proposes an innovative method for missile autopilot design based on the deep deterministic policy gradient (DDPG) algorithm. Under the framework of deep reinforcement learning, by integrating the missile’s dynamic characteristics to optimize the reward function and network structure, an adaptive control model capable of adapting to complex flight conditions was constructed. The effective integration of the autopilot and guidance system was achieved in the Simulink simulation environment, and the model’s validity and robustness in complex dynamic environments were verified. This research provides a new technological approach for the intelligent design of missile autopilots.

Authors

Institutions

Publication Details

Journal
International Journal of Aerospace Engineering
Published
2025-01-01
DOI
https://doi.org/10.1155/ijae/9542576
Primary Topic
Guidance and Control Systems
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Research on the Design and Simulation of Missile Intelligent Agent Autopilot Integrated With Deep Reinforcement Learning

Jianqi Wang, S S Wang, Shan Long, Kaiyu Zhan
International Journal of Aerospace Engineering
Guidance and Control Systems
article

Research on the Design and Simulation of Missile Intelligent Agent Autopilot Integrated With Deep Reinforcement Learning

Jianqi Wang, S S Wang, Shan Long, Kaiyu Zhan
article en

Abstract

This paper proposes an innovative method for missile autopilot design based on the deep deterministic policy gradient (DDPG) algorithm. Under the framework of deep reinforcement learning, by integrating the missile’s dynamic characteristics to optimize the reward function and network structure, an adaptive control model capable of adapting to complex flight conditions was constructed. The effective integration of the autopilot and guidance system was achieved in the Simulink simulation environment, and the model’s validity and robustness in complex dynamic environments were verified. This research provides a new technological approach for the intelligent design of missile autopilots.

International Journal of Aerospace EngineeringVol. 2025(1)
Harbin Institute of Technology (CN), Guilin University of Aerospace Technology (CN), Guilin University of Technology (CN), Guilin University of Electronic Technology (CN), Nanjing University of Aeronautics and Astronautics (CN)
Openalex Percentile: Top 75%
Guidance and Control Systems
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.