Sentence examples for attitude trajectory from inspiring English sources

The generalized dynamic inversion control methodology is applied to the spacecraft attitude trajectory tracking problem.

With the estimated values, a finite-time controller is further developed under which the time-varying reference attitude trajectory can be tracked precisely.

Thus the spacecraft in the formation are able to track the reference attitude trajectory even in the presence of time-varying communication delays.

The stability analysis demonstrates that the desired attitude trajectories are followed even in the presence of external disturbance and internal flexible modes.

In this paper, a time-varying control design is described that copes with magnetometer measurements, even in the case of rather general reference attitude trajectories.

We call such exception problems the attitude-trajectory or coupled problems.

This example deals with a minimum time maneuver of a coupled attitude-trajectory dynamic system.

In this section, we formulate an attitude-trajectory minimum time control problem, denoted by ((mathcal {P}_{S})).

In the next section, we will show step by step by a nonacademic attitude-trajectory problem how the analysis and the design of numerical continuation procedure are done.

In this section, the nonacademic attitude-trajectory optimal control problem for a launch vehicle (classical and airborne) is analyzed in detail.

In Section 7, we detail a full nonacademic example in aerospace (an attitude-trajectory problem), in order to illustrate how to solve optimal control problems with the help of geometric optimal control theory and the continuation methods.