Sentence examples for optimal attitude from inspiring English sources

This paper studies the active optimal attitude control of a three-axis stabilized flexible spacecraft by flywheels.

In addition, the masses associated with each observation vector can be adjusted to improve estimation accuracy and in many cases provide the optimal attitude estimate.

The optimal attitude control algorithms are validated on a microsatellite software simulator in collaboration with the space company Surrey Satellite Technology Limited SSTLL).

An optimal attitude control method based upon linear quadratic regulator is applied to a spacecraft in an inclined orbit, alternatively using magnetic torquers and reaction wheels.

Thus, this paper complements the previous mentioned work, and focuses on employing the H∞ optimal attitude control solution for the CEACS attitude control enhancement.

In this paper a robust and optimal attitude control design that uses the minimal kinematic parameters and angular velocities feedback is presented for the three-axis attitude stabilization of spacecraft with inertia uncertainties.

A nonacademic example of optimal attitude-trajectory control of (classical and airborne) launch vehicles, treated in details, illustrates how geometric optimal control can be used to analyze finely the structure of the extremals.

First, two optimal position and attitude controllers are developed to achieve asymptotic convergence to the desired position and attitude.

For the second control law, the optimal Lyapunov approach is used to design an optimal position and attitude controller.

Then robust optimal position and attitude controllers are designed by using an integral sliding mode control method to combine a second order sliding mode controller with the derived inverse optimal controller or optimal Lyapunov controller.

Third, the optimal camera attitude is updated based on the horizon with the designed Kalman filter.