Networking Attitude was designed to produce business successes, and it did.
And, of course, like all homophobia and all bigotry, these attitudes were designed to de-humanise me, to marginalise me and to keep me down.
By using the technique of finite-time saturation control, a bounded finite-time attitude controller is designed to track the estimated attitude and then the leader's attitude in a finite time.
The standard attitude estimator is designed to be optimal with respect to its absolute knowledge error.
In this paper, an autopilot for attitude tracking is designed using disturbance compensation techniques.
Then, an attitude control is designed from a linearization of the dynamic model around the hovering flight equilibrium.
Then, the attitude controller is designed by use of double loop scheme, the outer loop and the inner loop, which both track the command attitude angles and angular velocities.
A possible solution is that, after the attitude controller is designed on the nominal model, a Verification and Validation (V&V) process is performed to guarantee a correct functionality under a large number of scenarios.
First, a finite-time filter is proposed to generate the pseudo-angular-velocity signal, which is fed to the controller, and then a continuous finite-time attitude controller is designed based on the proposed filter.
The stability of the spacecraft's attitude, which is designed for the other cameras onboard Akatsuki, is within 0.015 deg (Nakamura et al., 2011).
