Full envelope missile longitudinal autopilot design using the state-dependent Riccati equation method

Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method

Nonlinear Problems in Aviation and Aerospace ◽

10.1201/9781482296914-12 ◽

2000 ◽

pp. 75-94

Keyword(s):

Riccati Equation ◽

The State ◽

Equation Method ◽

State Dependent

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Application of the state-dependent Riccati equation method in nonlinear control design for inverted pendulum systems

2013 IEEE 11th International Symposium on Intelligent Systems and Informatics (SISY) ◽

10.1109/sisy.2013.6662572 ◽

2013 ◽

Cited By ~ 2

Author(s):

Slavka Jadlovska ◽

Jan Sarnovsky

Keyword(s):

Nonlinear Control ◽

Riccati Equation ◽

Inverted Pendulum ◽

Control Design ◽

The State ◽

Equation Method ◽

State Dependent

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Control designs for the nonlinear benchmark problem via the state-dependent Riccati equation method

International Journal of Robust and Nonlinear Control ◽

10.1002/(sici)1099-1239(19980415/30)8:4/5<401::aid-rnc361>3.0.co;2-u ◽

1998 ◽

Vol 8 (4-5) ◽

pp. 401-433 ◽

Cited By ~ 180

Author(s):

Curtis P. Mracek ◽

James R. Cloutier

Keyword(s):

Riccati Equation ◽

The State ◽

Equation Method ◽

Benchmark Problem ◽

State Dependent ◽

Control Designs

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Non-linear optimal control of articulated-vehicle planar motion based on braking utilizing the state-dependent Riccati equation method

Proceedings of the Institution of Mechanical Engineers Part D Journal of Automobile Engineering ◽

10.1177/0954407015571156 ◽

2015 ◽

Vol 229 (13) ◽

pp. 1774-1787 ◽

Cited By ~ 4

Author(s):

Farzad Mobini ◽

Ali Ghaffari ◽

Mohsen Alirezaei

Keyword(s):

Optimal Control ◽

Riccati Equation ◽

The State ◽

Planar Motion ◽

Equation Method ◽

Linear Optimal Control ◽

State Dependent ◽

Articulated Vehicle ◽

Non Linear

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An analysis of the state dependent Riccati equation method nonlinear estimation technique

10.2514/6.2000-4275 ◽

2000 ◽

Cited By ~ 8

Author(s):

Craig Ewing

Keyword(s):

Riccati Equation ◽

Nonlinear Estimation ◽

The State ◽

Equation Method ◽

Estimation Technique ◽

State Dependent

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Observer design for satellite angular rate estimation using the state-dependent riccati equation method

IEEE Transactions on Aerospace and Electronic Systems ◽

10.1109/taes.2015.140159 ◽

2015 ◽

Vol 51 (3) ◽

pp. 2496-2501 ◽

Cited By ~ 6

Author(s):

Jaehyun Jin

Keyword(s):

Riccati Equation ◽

Angular Rate ◽

The State ◽

Observer Design ◽

Equation Method ◽

Rate Estimation ◽

State Dependent

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Nonlinear Control for Spacecraft Pursuit-Evasion Game Using the State-Dependent Riccati Equation Method

IEEE Transactions on Aerospace and Electronic Systems ◽

10.1109/taes.2017.2725498 ◽

2017 ◽

Vol 53 (6) ◽

pp. 3032-3042 ◽

Cited By ~ 10

Author(s):

Ashish Jagat ◽

Andrew J. Sinclair

Keyword(s):

Nonlinear Control ◽

Riccati Equation ◽

The State ◽

Equation Method ◽

Pursuit Evasion ◽

State Dependent ◽

Evasion Game

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A Suboptimal Tracking Control Approach Based on the State-Dependent Riccati Equation Method

Journal of Computational and Theoretical Nanoscience ◽

10.1166/jctn.2016.4740 ◽

2016 ◽

Vol 13 (1) ◽

pp. 1013-1021 ◽

Cited By ~ 2

Author(s):

Yong-Lin Kuo ◽

Tsung-Liang Wu

Keyword(s):

Riccati Equation ◽

Tracking Control ◽

The State ◽

Equation Method ◽

Control Approach ◽

State Dependent

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Analysis of Missile Longitudinal Autopilot Based on the State-Dependent Riccati Equation Method

Journal of Guidance Control and Dynamics ◽

10.2514/1.g003679 ◽

2019 ◽

Vol 42 (10) ◽

pp. 2183-2196

Author(s):

Jaeho Lee ◽

Namhoon Cho ◽

Youdan Kim

Keyword(s):

Riccati Equation ◽

The State ◽

Equation Method ◽

State Dependent

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Kinematically Coupled Relative Spacecraft Motion Control Using the State-Dependent Riccati Equation Method

Journal of Aerospace Engineering ◽

10.1061/(asce)as.1943-5525.0000436 ◽

2015 ◽

Vol 28 (4) ◽

pp. 04014099 ◽

Cited By ~ 7

Author(s):

Daero Lee ◽

Hyochoong Bang ◽

Eric A. Butcher ◽

Amit K. Sanyal

Keyword(s):

Riccati Equation ◽

Motion Control ◽

The State ◽

Equation Method ◽

Spacecraft Motion ◽

State Dependent

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