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