STABILITY AND PERFORMANCE ANALYSIS OF NONLINEAR AND NON-NORMAL SYSTEMS USING QUADRATIC CONSTRAINTS

von Kalur, Aniketh
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 3 of 7 (2020)

Feedback Stabilization of Incompressible Flows Using Quadratic Constraints

von Mushtaq, Talha
Veröffentlicht in AIAA Aviation Forum (2022 : Chicago, Ill.; Online) Fluid dynamics ; Volume 2 of 3 (2022)

RELIABILITY ANALYSIS FOR SMALL UNMANNED AIR VEHICLE WITH ALGORITHMIC REDUNDANCY

von Kotikalpudi, Aditya
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Unmanned systems (2020)

RELIABILITY OF ANALYTICALLY REDUNDANT SYSTEMS FOR SMALL UNMANNED AERIAL SYSTEMS

von Kotikalpudi, Aditya
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Unmanned systems ; Volume 2 of 2 (2021)

Structured Input-Output Tools for Modal Analysis of a Transitional Channel Flow

von Mushtaq, Talha
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Fluid dynamics ; Volume 5 of 6 (2023)

Structured Input-Output Analysis of Compressible Plane Couette Flow

von Bhattacharjee, Diganta
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Fluid dynamics ; Volume 5 of 6 (2023)

MAEWING2: INITIAL FLIGHT TEST AND SYSTEM IDENTIFICATION OF A FLEXIBLE UAV

von Regan, Christopher D.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Atmospheric flight mechanics ; Volume 2 of 2 (2020)

REAL-TIME SHAPE ESTIMATION FOR FLEXIBLE UNMANNED AIR VEHICLE VIA KALMAN FILTERING

von Kotikalpudi, Aditya
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Atmospheric flight mechanics ; Volume 2 of 2 (2020)

Are taxpayers increasing the buildup of retirement assets? : Preliminary results from a matched file of tax year 1999 tax returns and information returns

von Sailer, Peter J.
Veröffentlicht in Conference on Taxation (95 : 2002 : Orlando, Fla.) Proceedings (2003)