Combined Optimal/Classical Approach to Robust Missile Autopilot Design

Combined Optimal/Classical Approach to Robust Missile Autopilot Design

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Veröffentlicht in:Journal of guidance, control, and dynamics control, and dynamics, 1981-05, Vol.4 (3), p.316-322
Hauptverfasser: Nesline, F. William, Wells, Brian H, Zarchan, Paul
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Sprache:eng
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container_end_page 322
container_issue 3
container_start_page 316
container_title Journal of guidance, control, and dynamics
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creator Nesline, F. William
Wells, Brian H
Zarchan, Paul
description
doi_str_mv 10.2514/3.56084
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ispartof Journal of guidance, control, and dynamics, 1981-05, Vol.4 (3), p.316-322
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language eng
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source Alma/SFX Local Collection
title Combined Optimal/Classical Approach to Robust Missile Autopilot Design
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