Attitude Dynamics and Control of Space Debris During Ion Beam Transportation
Aslanov V.S., Ledkov A.S. "Attitude Dynamics and Control of Space Debris During Ion Beam Transportation," Elsevier,
2022, 309 p., Doi: 10.1016/C2021-0-02051-4, ISBN: 9780323992992
Аннотация
Acknowledgment
Introduction
Basics of space flight mechanics and control theory
1.1. Mathematical and mechanical preliminaries
1.2. Coordinate systems
1.3 Two-body problem: Motion in the orbital plane
1.4 Planetary equations for perturbed motion
1.5 Relative orbital motion
1.6 Rigid body attitude motion in orbit
1.7 Orbital and attitude perturbations
1.8 Lyapunov stability theory for the search for control laws
1.9 Chaotic dynamics of nonlinear system
Space debris problem
2.1 Review of the space debris problem
2.2 Contact methods of active space debris removal
2.3 Contactless space debris removal approaches
Ion beam physics
3.1 Mathematical modeling of an in-beam
3.2 Simplified ion beam models
3.3 Physics of ion beam interaction with a body surface
3.4 Calculating the forces and torque generated by the ion beam
3.5 Examples of ion force and torque calculations
Dynamics of relative translation motion of spherical space debris during ion beam transportation
4.1 Mathematical model describing ion beam transportation without taking into account space debris attitude motion
4.2 Calculation of fuel consumption and thruster plume parameters
4.3 Estimation of the thruster exhaust velocity and propellant mass for space debris deorbiting from a circular orbit
4.4 Active spacecraft relative position stability and control
4.5 Space debris removal: Preliminary mission design
Dynamics of passive object attitude motion during ion beam transportation
5.1 Mathematical models of a passive space debris object during its contactless transportation by an active spacecraft
5.2 Attitude dynamics of the uncontrolled motion of a passive space debris object at a constant relative position of the active spacecraft
5.3 Dynamics of the controlled motion of a passive object
5.4 Fuel costs estimation for ion beam-assisted space debris removal mission with and without attitude control
The use of contactless ion beam technology
6.1 Orbital flight in one plane
6.2 Deorbiting of space debris object into the atmosphere
6.3 Transportation of space debris into disposal orbit
About
Александр Сергеевич Ледков - доцент и старший научный сотрудник Института авиационной и ракетно-космической техники Самарского университета.