Nonlinear Robust Adaptive Control of Flexible Air-Breathing Hypersonic Vehicles
By L. Fiorentini, Andrea Serrani, M. Bolender, David B. Doman. 2009
573 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Control and Systems Engineering
View Paper: https://www.semanticscholar.org/paper/b13c14875248c8024d1eaaa106b452b1fd23ee43
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In Aerospace Engineering
In Control and Systems Engineering
Citations in the corpus
- Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle (2015, background): “In [17], the hypersonic flight dynamics is formulated into the linearly parameterized form.”
- Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future (2011, methodology): “The model includes the interaction of vehicle aerodynamics, propulsion, and structural dynamics, and it has been used for several [205–214] control design and simulation studies.”
- Nonlinear-Disturbance-Observer-Based Robust Flight Control for Airbreathing Hypersonic Vehicles (2013, methodology): “Based on the models obtained by approximate linearization around specified trim condition or input/output linearization technique, many advanced control methods, such as adaptive control [2], robust control [3—5, 7], sliding mode control [8], back-stepping control [9, 18], guaranteed cost control [1”
- Dynamic Surface Control of Constrained Hypersonic Flight Models with Parameter Estimation and Actuator Compensation (2014, methodology): “In [9,12,14,18], by functional decomposition, the velocity is independent of the other subsystems.”