While Deep Reinforcement Learning (DRL) offers robust real-time control for Active Debris Removal (ADR), current literature often assumes idealized dynamics and isolated mission segments. This paper presents an end-to-end 6 Degrees of Freedom (6-DOF) Guidance, Navigation, and Control (GNC) architecture using Proximal Policy Optimization (PPO) for a complete four-phase ADR mission. Bypassing standard linear approximations, the custom environment utilizes an absolute Keplerian N-Body Earth-Centered Inertial (ECI) propagator. It enforces operational realism through continuous Tsiolkovsky propellant dynamics, unmitigated kinematic handovers between phases, and instantaneous Huygens-Steiner inertia updates upon target capture. Trained via Curriculum Learning and astrodynamic energy rewards, the agent successfully executes fuel-optimized orbital transfers, performs dynamic obstacle avoidance, stabilizes proximity operations despite handover drift, and autonomously adapts to the severely degraded mass dynamics of the composite orbital vehicle.
A 6-DOF Deep Reinforcement Learning Architecture for Autonomous Debris Capture and Orbit Transfer / Falconi, F., Kamel, K.R.A., Menegatti, D., Delli Priscoli, F.. - (2026), pp. 2590-2595. (12th International Conference on Control, Decision and Information Technologies (CoDIT) Bari 13-16 July 2026) [10.1109/codit70676.2026.11630811].
A 6-DOF Deep Reinforcement Learning Architecture for Autonomous Debris Capture and Orbit Transfer
Kirolos Romany Anwar Kamel
Supervision
;Francesco Delli PriscoliSupervision
2026
Abstract
While Deep Reinforcement Learning (DRL) offers robust real-time control for Active Debris Removal (ADR), current literature often assumes idealized dynamics and isolated mission segments. This paper presents an end-to-end 6 Degrees of Freedom (6-DOF) Guidance, Navigation, and Control (GNC) architecture using Proximal Policy Optimization (PPO) for a complete four-phase ADR mission. Bypassing standard linear approximations, the custom environment utilizes an absolute Keplerian N-Body Earth-Centered Inertial (ECI) propagator. It enforces operational realism through continuous Tsiolkovsky propellant dynamics, unmitigated kinematic handovers between phases, and instantaneous Huygens-Steiner inertia updates upon target capture. Trained via Curriculum Learning and astrodynamic energy rewards, the agent successfully executes fuel-optimized orbital transfers, performs dynamic obstacle avoidance, stabilizes proximity operations despite handover drift, and autonomously adapts to the severely degraded mass dynamics of the composite orbital vehicle.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

