Angular Momentum Device for Stabilization and Control for Tailless Aircraft

Non-Confidential description of the invention

This invention relates to an angular momentum device/system for stabilization and control for tailless aircraft. The device/system provides additional dynamic coupling between rolling and yawing motions of the aircraft. Our invention provides an angular momentum system for improving the dynamics, stability and controllability of tailless aircraft. The angular momentum system improves directional stability or allows the controller to influence more strongly the directional dynamics, of aircraft without vertical surfaces.

Inventors

Mr. Vishvendra Rustagi (Student, AE), Dr. Anindya Chatterjee(ME), Dr. Mangal Kothari(AE)

IPA

201711017649

Date of Filing

19/05/2017

Status

Date Of Grant

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