Dynamic trajectory control of gliders
Rui Dil\~ao, Jo\~ao Fonseca
TL;DR
This paper introduces a new iterative dynamic control algorithm for guiding gliders to a target point, demonstrating its application on Space Shuttle trajectory control during TAEM.
Contribution
The paper presents a novel self-correcting control algorithm applicable to any non-powered lift-enabled vehicle in planetary atmospheres.
Findings
Algorithm successfully guides a glider to a target point
Applied to Space Shuttle trajectory control during TAEM
Demonstrates potential for planetary atmospheric vehicle navigation
Abstract
A new dynamic control algorithm in order to direct the trajectory of a glider to a pre-assigned target point is proposed. The algorithms runs iteratively and the approach to the target point is self-correcting. The algorithm is applicable to any non-powered lift-enabled vehicle (glider) travelling in planetary atmospheres. As a proof of concept, we have applied the new algorithm to the command and control of the trajectory of the Space Shuttle during the Terminal Area Energy Management (TAEM) phase.
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Taxonomy
TopicsSpace Satellite Systems and Control · Spacecraft Dynamics and Control