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Alternate forms of relative attitude kinematics and dynamics equations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Parvez, Shabbir A. Xing, Guang Q. |
| Copyright Year | 2001 |
| Description | In this paper the alternate forms of the relative attitude kinematics and relative dynamics equations are presented. These developments are different from the earlier developments that have been presented in other publications. The current forms of equations have the advantage of being simpler than earlier ones. These equations are applied in developing the necessary kinematics and dynamics for relative navigation in formation flying and virtual platforms. These equations also have application in the implementation of nonlinear full state feedback and nonlinear output feedback control for large attitude angle acquisition and tracking. This paper presents simulations from such a full state feedback control application. |
| File Size | 454361 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20010084965 |
| Archival Resource Key | ark:/13960/t2c877p7d |
| Language | English |
| Publisher Date | 2001-06-01 |
| Access Restriction | Open |
| Subject Keyword | Astrodynamics Nonlinear Feedback Spacecraft Control Attitude Inclination Computerized Simulation Feedback Control Kinematics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
