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control systems
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Measurement of autogyro control forces
Performance analysis of trailing-edge flaps in helicopter primary control
Quantitative feedback theory (QFT) applied to the design of a rotorcraft flight control system
On power and actuation requirement in swashplateless primary control using trailing-edge flaps
Flapping equals feathering. Aerodynamics
Ein Beitrag zur Modellierung und Identifizierung eines schubvektorgesteuerten Flugzeugs
Mensch-Maschine-Schnittstelle für entfernungsabtastende Sensoren zukünftiger Hubschrauber
Tail rotor failures, part 2. Aerodynamics
The T-Wing tail-sitter unmanned air vehicle: From design concept to research flight vehicle
Development and evaluation of an integrated flight and propulsion control system
Tail-rotor failures, part 1. Aerodynamics
A parametric design study for a swashplateless helicopter rotor with trailing-edge flaps
The application of actuator performance limits to aeroservoelastic compensation
The new DLR flight dynamics library
Lastannahmen und Sicherheit. Auslegung und Nachweisführung von Flugzeugstrukturen
Robust multivariable control of rotorcraft in forward flight: Impact of bandwidth on fatigue life
Fuselage state feedback for aeromechanical stability augmentation of a bearingless main rotor