D.T. Stansbery

Position and attitude control of a spacecraft using the state-dependent Riccati equation technique

D.T. Stansbery, J.R. Cloutier · 2000 · 164 citations

Space Vehicle, Engineering, Attitude Control +12

The capabilities and art of state-dependent Riccati equation-based design

J.R. Cloutier, D.T. Stansbery · 2003 · 160 citations · Full text

Nonlinear Control, Nonlinear System Identification, Engineering +10

Nonlinear Missile Autopilot Design with Theta-D Technique

Ming Xin, S.N. Balakrishnan, D.T. Stansbery et al. · Journal of Guidance Control and Dynamics · 2004 · 101 citations

Missile, Flight Control Systems, θ − D +13

Nonlinear, hybrid bank-to-turn/skid-to-turn missile autopilot design

D.T. Stansbery, J.R. Cloutier · AIAA Guidance, Navigation, and Control Conference and Exhibit · 2001 · 52 citations

Missile, Bank Angle, Engineering +16

Control of a continuously stirred tank reactor using an asymmetric solution of the state-dependent Riccati equation

J.R. Cloutier, D.T. Stansbery · 2003 · 39 citations

Nonlinear Control, Process Design, State Weighting Matrix +12