Research Integrated Guidance Control Design is a M.Tech project topic for Aerospace Engineering. It gives students a clear starting point for research, implementation planning, and documentation.
Research Integrated Guidance Control Design Project Details
| Abstract |
The conventional methods for missile guidance are system dependent and thus, face limitations with regard to adaptability and flexibility in targeting highly maneuverable targets. This study offers an answer to this problem with the integrated guidance and control (IGC) approach using the Twin Delayed Deep Deterministic Policy Gradient (TD3) algorithm. The author describes the three-dimensional interception problem with a roll-free, two-channel missile system as a Markov decision process (MDP). He then trains an end-to-end policy to simplify the control architecture by mapping observed engagement states to control surface deflection commands directly. The LOS (line-of-sight) rate is the central focus because the learning process is structured around a multi-component reward function
and achieving convergence to stable terminal guidance. The IGC method based on TD3 approaches the performance of standard three-channel proportional navigation (PN) systems in all simulations. Additionally, when tested against continuously evasive maneuvering targets that have not been included in the training dataset, the method performed exceptionally well and maintained a high interception accuracy in contrast to conventional systems. This demonstrates the framework’s ability to be generalized for potential use in real scenarios that are complex and challenging.
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| Reference Paper |
Research on an Integrated Guidance and Control Design Method for Missiles Based on TD3 |
| Domain |
Aerospace Engineering |
| Sub-Domain |
Structures & Systems / Guidance Navigation Control / Autopilot Design |
| PDF Download |
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| Get Help |
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