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Gokhan Inalhan

Researcher at Cranfield University

Publications -  132
Citations -  2901

Gokhan Inalhan is an academic researcher from Cranfield University. The author has contributed to research in topics: Computer science & Trajectory. The author has an hindex of 20, co-authored 102 publications receiving 2539 citations. Previous affiliations of Gokhan Inalhan include Massachusetts Institute of Technology & Istanbul Technical University.

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Journal ArticleDOI

Decentralized overlapping control of a formation of unmanned aerial vehicles

TL;DR: Decentralized overlapping feedback laws are designed for a formation of unmanned aerial vehicles based on the application of convex optimization tools involving linear matrix inequalities to robustly stabilize the perturbed nominal dynamics of the subsystem.
Journal ArticleDOI

Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits

TL;DR: In this paper, a complete initialization procedure for a large fleet of vehicles with an eccentric reference orbit is presented, which minimizes the fuel cost associated with initializing the vehicle states (primarily the in-track and radial relative velocities) to values consistent with periodic relative motion.
Proceedings ArticleDOI

Decentralized optimization, with application to multiple aircraft coordination

TL;DR: A globally convergent algorithm based on sequential local optimizations is presented that results in global convergence to /spl epsiv/-feasible Nash solutions that satisfy the Karush-Kuhn-Tucker necessary conditions for Pareto-optimality.
Journal ArticleDOI

Co-ordination and control of distributed spacecraft systems using convex optimization techniques

TL;DR: In this paper, the authors present fuel/time-optimal control algorithms for a co-ordination and control architecture that was designed for a fleet of spacecraft, including low-level formation-keeping algorithms and a high-level fleet planner that creates trajectories to re-size or re-target the formation.
Journal ArticleDOI

Design of a Commercial Hybrid VTOL UAV System

TL;DR: The preliminary design process of such a capable civilian UAV system, namely the TURAC VTOL UAV, is reviewed, which is aimed to have both vertical take-off and landing and Conventional Take-offs and Landing (CTOL) capability.