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Youmin Gong

Assistant professor

Harbin Institute of Technology

China

Research Interests

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Articles (20)

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2027

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2026

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2026

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2025

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2025

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2024

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2024

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2024

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2024

Collaborators (3)

James Lam

Chair Professor of Control Engineering

The University of Hong Kong

HONG KONG

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Edoardo Fadda

Personale esterno ed autonomi

Politecnico di Torino

ITALY

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Yanning Guo

Professor

Harbin Institute of Technology

CHINA

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ApplyKite TwinLearns as you apply

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Youmin Gong

Research Interests

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Articles (20)

Physics-constrained maximum entropy inverse reinforcement learning with learned-cost rollout for spacecraft pursuit evasion in elliptical orbits

Obstacle avoidance guidance for Mars powered descent using convex optimization and elevation angle

Covariance Steering for Powered-Descent Guidance with Embedded Navigation and Tracking

Decentralized End-to-End Multi-AAV Pursuit Using Predictive Spatio-Temporal Observation via Deep Reinforcement Learning

Adaptive State Consensus of Uncertain MIMO Dynamical Multiagent Systems via Output Feedback Over a Directed Graph

Optimal Control of Spacecraft Formation With Predefined Performance via Extended State Method

Robust powered descent guidance considering mass and fuel consumption uncertainties: A convex optimization approach

Optimized Fault‐Tolerant Fixed‐Time Control for Nonlinear Strict‐Feedback Systems With Output Constraints

Adaptive Near-Propellant-Optimal Powered Descent Initiation for Human Mars Landing

Deep reinforcement learning-based fast hybrid planning for multi-type on-orbit service under mass variation dynamics

Anti-Unwinding Time-Varying Sliding Mode Control With Arbitrary Convergence Time for Rigid Spacecraft

Distributed Leaderless Attitude Consensus of Multispacecraft Systems With Full-State Constraints Under Switching Directed Graphs

Future-Trend-Aware Filter-Based PD-MRAC Method for Quadrotors With Unknown Strong Disturbances

Augmented-Zero-Effort-Miss/ Zero-Effort-Velocity Guidance With Adaptive Collision Avoidance

Collision-Free Approximate Optimal Control of Spacecraft Formation With Predefined Performance

Robust optimal powered descent guidance via model predictive convex programming

Adaptive pseudospectral successive convex optimization for six-degree-of-freedom powered descent guidance

Hybrid Zero-Effort-Miss/Zero-Effort-Velocity Guidance for Powered Descent Phase

Path and control-constrained longitudinal guidance for Mars entry

Fast fixed-time three-dimensional terminal guidance with non-concave trajectory constraint

Collaborators (3)

James Lam

Edoardo Fadda

Yanning Guo

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