Loading...
Please wait, while we are loading the content...
Output attitude tracking of a formation of spacecraft
| Content Provider | Semantic Scholar |
|---|---|
| Author | Grøtli, Esten Ingar Gravdahl, Jan Tommy |
| Copyright Year | 2008 |
| Abstract | This paper will consider the control of spacecraft in a leader-follower formation using attitude measurements only. To analyze the formation under non vanishing disturbances, the concept of uniform practical exponential stability is defined. To ease the Lyapunov analysis a new theorem is provided, giving sufficient conditions for systems that present a cascaded structure to satisfy this definition. Finally, output control is applied to both the leader and follower spacecraft and the stability of the overall system is analyzed through the application of this new result. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://folk.ntnu.no/skoge/prost/proceedings/ifac2008/data/papers/3864.pdf |
| Alternate Webpage(s) | http://www.itk.ntnu.no/ansatte/Gravdahl_Jan.Tommy/papers/ifac2008_Gr%EF%BF%BDtli.pdf |
| Language | English |
| Access Restriction | Open |
| Subject Keyword | Computer simulation Convergence (action) Kind of quantity - Equilibrium Lyapunov fractal Multiple encryption Rate of convergence Reasoning Solutions Spacecraft exponential |
| Content Type | Text |
| Resource Type | Article |
