3D Nonlinear H<sub>2</sub>/H<sub>1</sub> Guidance Law.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 277
- By:
- Publication type:
- Article
Works matching IS 13598678 AND DT 2004 AND VI 11 AND IP 2
Results: 9
1
2
Synthesis of missile gain-scheduled autopilots using an H∞-LPV technique with piecewise continuously differentiable parameter-dependent Lyapunov functions.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 243
- By:
- Publication type:
- Article
3
Model Following Control Approach for Missile Autopilot Design.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 227
- By:
- Publication type:
- Article
4
Missile Autopilot Design via Approximate Nonlinear Dynamic Inversion.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 215
- By:
- Publication type:
- Article
5
Reduced order H∞ loop-shaping control of a missile pitch axis over a wide flight envelope.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 199
- By:
- Publication type:
- Article
6
Computer-Aided Synthesis of Nonlinear Autopilot for Missiles.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 173
- By:
- Publication type:
- Article
7
An LFT approach to scheduled feedback design with an application to the synthesis of a missile autopilot.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 157
- By:
- Publication type:
- Article
8
Multi-objective Fuzzy Design of a Lateral Autopilot for a Quasi-Linear Parameter Varying Missile.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 135
- By:
- Publication type:
- Article
9
Control in Defence Systems.
- Published in:
- Nonlinear Studies, 2004, v. 11, n. 2, p. 131
- By:
- Publication type:
- Article