Determining Follower Aircraft's Optimal Trajectory in Relation to a Dynamic Formation Ring
Carl A. Gotwald, Michael D. Zollars, and Isaac E. Weintraub

TL;DR
This paper develops a numerical tool to compute optimal trajectories for follower aircraft to rejoin and maintain a formation ring around a leader, considering aircraft dynamics, constraints, and avoiding jet wash.
Contribution
The paper introduces a novel optimal control framework using GPOPS-II for trajectory planning of follower aircraft in formation rejoin scenarios.
Findings
Trajectories show direct capture of formation position.
Solver initial conditions affect trajectory behaviors.
The tool supports future real-time controller development.
Abstract
The specific objective of this paper is to develop a tool that calculates the optimal trajectory of the follower aircraft as it completes a formation rejoin, and then maintains the formation position, defined as a ring of points, until a fixed final time. The tool is designed to produce optimal trajectories for a variety of initial conditions and leader trajectories. Triple integrator dynamics are used to model the follower aircraft in three dimensions. Control is applied directly to the rate of acceleration. Both the follower's and leader's velocities and accelerations are bounded, as dictated by the aircraft's performance envelope. Lastly, a path constraint is used to ensure the follower avoids the leader's jet wash region. This optimal control problem is solved through numerical analysis using the direct orthogonal collocation solver GPOPS-II. Two leader trajectories are…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Distributed Control Multi-Agent Systems · Guidance and Control Systems
