Dynamics and Stability of an Autorotating Rotor/Wing Unmanned Aircraft

C. A. Lopez, Valana Wells

Research output: Contribution to journalArticle

13 Citations (Scopus)

Abstract

The development of and results from a dynamic analysis of a hybrid autorotating rotor/wing aircraft are presented. The aircraft is intended for use as an unmanned reconnaissance vehicle to be air launched from the pylon of a base aircraft. The rotor/wing aircraft may be operated as a conventional, fixed-wing airplane or as an autogyro for low-speed surveillance and landing. Analysis presented includes dynamic stability and control features of the autogyro configuration. Generally, the autogyro exhibits dynamic modes characteristic of a conventional aircraft with the exception of an additional, slowly convergent mode associated with the rotor angular velocity degree of freedom. The rotor angular velocity also plays an important role in the unstable autogyro phugoid mode. Control effectiveness in the autorotating configuration is generally good, though it is recommended that the rotor longitudinal cyclic control be assisted by the elevons to enhance control power in pitch.

Original languageEnglish (US)
Pages (from-to)258-270
Number of pages13
JournalJournal of Guidance, Control, and Dynamics
Volume27
Issue number2
StatePublished - Mar 2004

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wings
Rotor
rotors
aircraft
Aircraft
Rotors
Angular velocity
angular velocity
military air facilities
elevons
Elevons
pylons
unmanned vehicle
fixed wings
Unmanned Vehicles
Fixed wings
dynamic stability
dynamic control
Configuration
reconnaissance

ASJC Scopus subject areas

  • Aerospace Engineering
  • Instrumentation

Cite this

Dynamics and Stability of an Autorotating Rotor/Wing Unmanned Aircraft. / Lopez, C. A.; Wells, Valana.

In: Journal of Guidance, Control, and Dynamics, Vol. 27, No. 2, 03.2004, p. 258-270.

Research output: Contribution to journalArticle

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