53 research outputs found
Quaternion Regularization of the Equations of the Perturbed Spatial Restricted Three-Body Problem: II
No full textThe problem of optimal control of the orientation of an orbit of a spacecraft as a deformable figure
No full textPulsed Optimal Spacecraft Orbit Reorientation by Means of Reactive Thrust Orthogonal to the Osculating Orbit. II
No full textThe problem of rendezvous of a controlled space vehicle with an uncontrolled space vehicle moving along an elliptical Keplerian orbit in the central Newtonian gravitational field
No full textQuaternion Regularization of the Equations of the Perturbed Spatial Restricted Three-Body Problem: I
No full textAnalysis of optimal motion control for a material point in a central field with application of quaternions
No full textOptimal reorientation of spacecraft orbit
No full textThe problem of optimal reorientation of the spacecraft orbit is considered. For solving the problem we used quaternion equations of motion written in rotating coordinate system. The use of quaternion variables makes this consideration more efficient. The problem of optimal control is solved on the basis of the maximum principle. An example of numerical solution of the problem is given
- …
