Sentence examples for attitude control strategy from inspiring English sources

An effective attitude control strategy is presented where the commands are optimized first and then feedback controller is designed.

The rest of the manuscript is organized as follows: the proposed cascade attitude control strategy is first given in "The proposed cascade attitude control strategy" section.

The attitude control strategy combines bang-bang and PD control, with constraints such as power consumption, response time, and stability factored into the optimality computations and a possible extension to PID control to account for disturbances.

A high-precision full quaternion based finite-time three-axis cascade attitude control strategy is considered in the present research with respect to state-of-the-art to deal with a class of overactuated space systems.

Finally, the proposed approach is applied to the definition of a preliminary attitude control strategy for the AMS-02 mission and its performance is compared with the one attainable using a classical three-axis state feedback controller.

The analysis is the basis for the design of an attitude control strategy that allows to minimize the required control torque while satisfying an absolute pointing error constraint whenever direct compensation of magnetic disturbance torque is not achievable.

Secondly, a novel attitude control scheme is developed and the control strategy consists of two parts to achieve a stable and accurate attitude tracking during reentry flight process.

This paper considers the problem of attitude synchronization for a group of flexible spacecraft based on distributed attitude cooperative control strategy.

To solve the problem of attitude synchronization for a group of flexible spacecraft during formation maneuvers, a distributed attitude cooperative control strategy is investigated in this paper.

Then, an active fault tolerant tracking strategy for RLV attitude control systems is presented by making use of both adaptive control and sliding mode control techniques, which can guarantee the asymptotic output tracking of the closed-loop attitude control systems in spite of actuator fault.

This paper introduces an observer-based sliding mode control strategy for stabilizing the attitude of flapping micro-air vehicles in the presence of unknown uncertainties and external disturbances.