On the dynamics of spinning tethered space vehicles

Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences

Volumn 359, Issue 1788, 2001, Pages 2161-2190

  Tyc, G ^a   Han, R P S ^a  

^a Bristol Aerospace Limited   (Canada)

Author keywords

Dynamics of spinning tethers; Spinning space tethers; Tethered systems

Indexed keywords

EID: 57249088447     PISSN: 1364503X     EISSN: None     Source Type: Journal    
DOI: 10.1098/rsta.2001.0881     Document Type: Article

References (46)

1. Active and passive damping of tethered systems
2. Results of TiPS flight dynamics investigations
3. Gravity-gradient effects on the motion of two rotating cable-connected bodies
4. Gravity-gradient excitation of a rotating cable-counterweight space station in orbit
5. Simulation technology developed at alenia spazio for dynamics analysis of tethered satellite systems
6. Development of software for the dynamic analysis of tethered systems
7. Dynamical analysis of tethered systems. Phase 2. Mathematical formulation and solution procedure. Final report
8. Design of the OEDIPUS-C suborbital payload
9. Atmospheric research using tethered satellite systems in elliptical orbits
10. Why space stations?
11. Tether damping in space
12. Asymptotic stability of linear mechanical systems
13. Flight results from the OEDIPUS-A tethered experiment
14. Plasma motor generator mission report
15. On the dynamics and control of N-body tethered systems
16. Operations with tethered space vehicles
17. Dynamics and control of the tether elevator/crawler system
18. SEDS-2 Deployment control law and mission design
19. Analytical vibration and resonant motion of a stretched spinning nonlinear tether
20. Plasma motor-generator (PMG) flight experiment results
21. Dynamics and control of tether connected two-body systems. A brief review
22. A survey of the dynamics and control of tethered satellite systems
23. Strings
24. The NASA/ASI TSS-1 Mission: Summary of results and reflight plans
25. Sounding rocket tethered payload experiments: The NASA charge program
26. The first and second flights of the small expendable deployer system (SEDS)
27. Dynamics of a space tether satellite system with two rigid bodies
28. TSS Mission 1 flight dynamic anomalies
29. OEDIPUS-A attitude determination study using magnetometer data
30. Attitude dynamics investigation of the OEDIPUS-A tethered rocket payload
31. Tether dynamics investigations for the Canadian OEDIPUS sounding rocket program
32. Dynamics and stability of a spinning tethered spacecraft with flexible appendage
33. Design of an attitude stabilization system for the OEDIPUS-C tethered rocket payload
34. Flight dynamics results from the OEDIPUS-C tether mission
35. Stability of a freely spinning satellite of crossed dipole configuration
36. Space tether technology in future Canadian programs