Yedavalli, Rama K. - Department of Aerospace Engineering, Ohio State University

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Yedavalli, Rama K. - Department of Aerospace Engineering, Ohio State University

Robustness Study of the Dynamic Inversion Based Indirect Adaptive Control of Flight Vehicles with Uncertain Model Data
Dynamic Inversion via State Dependent Riccati Equation Approach: Application to Flight Vehicles
Stability Domain Estimation for Dynamic Inversion Embedded SDRE Flight Controller
The sign stability gain for the following closed loop sign stable State space representation of
Stability Check Of Matrix Families: How And Why Vertex Solution For Multiple Vertex Case Is Different From Two Vertex