Multiple-spacecraft reconfiguration through collision avoidance, bouncing, and stalemate

DOI10.1023/B:JOTA.0000042524.57088.8bzbMath1092.70020OpenAlexW2025408923MaRDI QIDQ702377

Fred Y. Hadaegh, Mehran Mesbahi, Yoonsoo Kim

Publication date: 17 January 2005

Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/b:jota.0000042524.57088.8b

zbMATH Keywords

heuristic algorithmscollision avoidancebouncingMultiple-spacecraft reconfigurationstalematestate-constrained optimal control

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Control of mechanical systems (70Q05) Existence theories for optimal control problems involving partial differential equations (49J20) Orbital mechanics (70M20) Discrete approximations in optimal control (49M25)

Related Items (4)

Coordination and collision avoidance for Lagrangian systems with disturbances ⋮ A necessary and sufficient condition for the controllability of single-leader multi-chain systems ⋮ Real-time path planning with limited information for autonomous unmanned air vehicles ⋮ Markov Chain Approach to Probabilistic Guidance for Swarms of Autonomous Agents

Uses Software

• Optimization Toolbox

Cites Work

• A generalized gradient method for optimal control problems with inequality constraints and singular arcs
• Conflict resolution for air traffic management: a study in multiagent hybrid systems
• Unnamed Item

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