A signal-based H-infinity gain-scheduled cascaded attitude controller with feedforward filter is synthesized for an INDI-controlled quadrotor and shown to maintain acceptable tracking in nonlinear simulations and flight tests even when identified parameters fall outside the modeled uncertainty set,
Commande Robuste Structur ´ee : Application Co-Design M ´ecanique / Contr ˆole d’Attitude d’un Satellite Flexible
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Robust $\mathcal{H}_\infty$ Controller Design For INDI-Controlled Quadrotor Using Online Parameter Identification
A signal-based H-infinity gain-scheduled cascaded attitude controller with feedforward filter is synthesized for an INDI-controlled quadrotor and shown to maintain acceptable tracking in nonlinear simulations and flight tests even when identified parameters fall outside the modeled uncertainty set,