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Missile Autopilot Design using Adaptive Nonlinear Dynamic
| Content Provider | Semantic Scholar |
|---|---|
| Author | Hindman, Rick Shell, William M. |
| Copyright Year | 2005 |
| Abstract | This paper describes the continuing project Adap- tive Nonlinear Dynamic Inversion (ANDI). The ANDI autopilot uses non-linear dynamic inversion with an adaptive element to account for any errors in the inversion. A reference model is included to provide the desired output performance. This allows the missile performance to be tuned by simply adjusting the reference model parameters. This will result in a design that is robust with respect to aerodynamic modeling inaccuracies and to extenal disturbances. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://folk.ntnu.no/skoge/prost/proceedings/acc05/PDFs/Papers/0699_FrA16_3.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
