1 / 20

SPIN STABILILIZATION

Z. z. x. y. Y. X. y. Y. Z. z. X. x. SPIN STABILILIZATION. 1. INTRODUCTION Dynamics, Astrodynamics Orbital Dynamics, Attitude Dynamics Basic terminology Attitude. H. . Z. H. . Y. X. Spin stabilization. Single Spinners. Dual Spinners. H. . z,p. z. z. H. .

naiya
Télécharger la présentation

SPIN STABILILIZATION

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Z z x y Y X y Y Z z X x SPIN STABILILIZATION • 1. INTRODUCTION • Dynamics, Astrodynamics • Orbital Dynamics, Attitude Dynamics • Basic terminology • Attitude

  2. H  Z H  Y X • Spin stabilization

  3. Single Spinners Dual Spinners

  4. H  z,p z z H  H, ,p x x x y y y • 2. The Euler’s Moment Equations • Rigidy body dynamics: rotational motion in space • Torque-free motion • Reference systems: • geometrical • Angular momentum axis • instantaneous rotation axis • principal axes Pure rotation Conning Nutation

  5. z dm O x y Torque-free motion

  6. Spin stabilization with passive/active control

  7. Major Axis Rule for Spin Stabilization • Stability of rotation about principal axes • Consider the the perturbed the steady motion given • by the Euler’s moment equation for torque-free motion: Differentating w.r.t. time and eliminating

  8. Differentating w.r.t. time and eliminating Both of these equations represent simple harmonic oscillator with general solution: Where If  is imaginary jwill diverge andis unstable.  must be real for stability. This is satisfied when (Ix-Iy)(Ix-Iz) > 0 . Motion is stable when Ix>Iy e Ix>Iz or when Ix<Iy e Ix<Iz Conclusion: motion is stable about major or minor axis but motion about intermediate axis is unstable.

  9. Internal Energy Dissipation Effects • All real spacecraft have, at least, some nonrigid properties. • These include: elastic structural deflection and sloshing. • Some lessons learned from the past: • Explorer I (1958)

  10. Energy dissipation Since for torque-free motion the angular momentum must be conserved motion about the major axis corresponds to the minimum energy state. Conclusion: a semirigid body is stable only when spinning about the major axis, bringing about the major axis rule for spin stabilization.

  11. ATS-5 Satellite - 1969

  12. Adverse Effect Control System Probable Cause Year Satellite Spin Stabilized Internal Energy dissipation 1958 Explorer I Unstable Spin Stabilized Rapid Spin Decay Solar Torque on Thermally Deformed Satellite 1952 Alouette Solar Torque on Thermally Deformed Satellite Explorer XX Spin Stabilized Rapid Spin Decay 1964 Internal Energy Dissipation Spin Stabilized with active Nutation Control Unstable 1969 ATS-5 Examples of Flexibility and/or Dissipation Effects

  13. F R Momentum precession and spin thrusters locations

  14. Nutation Damper Torque coil SACI-1: Spin Stabilized with Geomagnetic Control

  15. SCD-1: Spin Stabilized Partially Filled Ring Nutation Damper Torque Coil

  16. Nutation damper Spin plane coils SACI-2 Spin stabilized with geomagnetic control Partially filled ring Nutation Damper

  17. Mathematical model: Satellite With a Partially Filled Ring Nutation Damper to Prevent Nutation Motion

  18. z Hz  H Hy Hx HT x y Computer Simulation

  19. Conclusion Directional Stability: inertial pointing Gyroscopic properties of rotating bodies Major axis rule: rigid body are only idealizations Single and Dual Spinners Nutation Dampers: passive and active Spin stabilization combined with active control

More Related