Pages that link to "Item:Q900318"
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The following pages link to Optimal reorientation of a Spacecraft's orbit using a jet thrust orthogonal to the orbital plane (Q900318):
Displaying 10 items.
- The problem of optimal control of the orientation of an orbit of a spacecraft as a deformable figure (Q734022) (← links)
- Optimal reorientation of a Spacecraft's orbit using a jet thrust orthogonal to the orbital plane (Q900318) (← links)
- Switching time-optimal control of spacecraft equipped with reaction wheels and gas jet thrusters (Q1642343) (← links)
- Threshold absolute value of a relay control when time-optimally bringing a satellite to a gravitationally stable position (Q1735290) (← links)
- Optimal rotation of the orbit plane of a variable mass spacecraft in the central gravitational field by means of orthogonal thrust (Q2289036) (← links)
- The optimal in terms of fuel consumption approach to reorientation of a spacecraft based on the nonlinear boundary value problem solution (Q2679185) (← links)
- Quaternion methods and regular models of celestial mechanics and space flight mechanics: the use of Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. I: Review and analysis of methods and models and their applications (Q2695821) (← links)
- Quaternion methods and regular models of celestial and space flight mechanic: using Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. II: Perturbed spatial restricted three-body problem (Q2699160) (← links)
- Optimal Reorientation Of Spacecraft Orbit (Q3453359) (← links)
- Influence of steering angle profiles on the orbit transfer trajectory (Q6484319) (← links)