D. T. Stansbery

Dynamic conversion of flight path angle commands to body attitude commands

J. R. Cloutier, D. T. Stansbery, 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).

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

D. T. Stansbery, J. Cloutier, 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).

Nonlinear Control of Satellite Formation Flight

D. T. Stansbery, J. Cloutier, 2000 .

State-dependent Riccati equation solution of the toy nonlinear optimal control problem

D. T. Stansbery, J. Cloutier, C. Mracek, 1998, Proceedings of the 1998 American Control Conference. ACC (IEEE Cat. No.98CH36207).

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

J. R. Cloutier, D. T. Stansbery, 1999, Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328).

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

J. R. Cloutier, D. T. Stansbery, J. Cloutier, 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).

On the recoverability of nonlinear state feedback laws by extended linearization control techniques

Mario Sznaier, J. R. Cloutier, D. T. Stansbery, 1999, Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251).

Nonlinear Missile Autopilot Design with theta - D Technique

Ming Xin, Ernest J. Ohlmeyer, S. N. Balakrishnan, 2004 .