author: quanmin zhu

... axis desired control torque (b) Z-axis actual control torque (c) Z-axis control torque error (a) Pitch angle error (b) Yaw angle error (c) Roll angle error Fig. 5 Rocket attitude angle error diagram with 90% thrust reduction (a) Z-axis ...

... systems. Autom Remote Control 3(1), 36–44 (1985) Nordfeldt, P., Hagglund, T.: Decoupler and PID controller design of TITO systems.JProcess Control 16(9), 923–936 (2006) Ogata, K.: Discrete time control systems, 2nd edn. Prentice Hall ...

... using the Jacobian transpose matrix such that: t = Mos-J' (0)(kie, + k2é,) – J' (0) ... delayed acceleration input computed using the following approximation: 6(t) ... technique (Reyes-Sierra and Coello 2005). Consider the Lyapunov function ...

... Trenchless Technology Magazine (2015) 5. Bugbee, K.P., Patton, B.D., Jubin, R.T. Robinson, S.M., Sullivan, N.M.: Evaluation of trenchless technologies for installation of pipelines in radioactive environments. In: Waste Management ...

... < R4 and R3 > R4, respectively. For the narrowband noise, the proposed system can achieve the aim of the cancellation ... passing is longer than the path for the primary source passing, the secondary source will be later when arriving at ...