Title:
Adaptive, Integrated Guidance and Control Design for Line-of-Sight-Based Formation Flight
Adaptive, Integrated Guidance and Control Design for Line-of-Sight-Based Formation Flight
| dc.contributor.author | Kim, Byoung Soo | |
| dc.contributor.author | Calise, Anthony J. | |
| dc.contributor.author | Sattigeri, Ramachandra J. | |
| dc.contributor.corporatename | Georgia Institute of Technology. School of Aerospace Engineering | |
| dc.contributor.corporatename | Gyeongsang National University | |
| dc.date.accessioned | 2010-11-10T18:14:57Z | |
| dc.date.available | 2010-11-10T18:14:57Z | |
| dc.date.issued | 2007-10 | |
| dc.description | Published in Journal of Guidance Control and Dynamics, Vol. 30, No. 5, September–October 2007. | en_US |
| dc.description | Presented as Paper 6716 at the AIAA Guidance Navigation and Control Conference and Exhibit, Keystone, Colorado, 21–24 August 2006; received 11 September 2006; revision received 9 April 2007; accepted for publication 26 April 2007. Copyright © 2007 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. | |
| dc.description.abstract | This paper presents an integrated guidance and control design for formation flight using a combination of adaptive output feedback and backstepping techniques. We formulate the problem as an adaptive output feedback control problem for a line-of-sight-based formation flight configuration of a leader and a follower aircraft. The design objective is to regulate range and two bearing angle rates while maintaining turn coordination. Adaptive neural networks are trained online with available measurements to compensate for unmodeled nonlinearities in the design process. These include uncertainties due to unknown leader aircraft acceleration, and the modeling error due to parametric uncertainties in the aircraft aerodynamic derivatives. One benefit of this approach is that the guidance and flight control design process is integrated. Simulation results using a nonlinear 6 degrees-of-freedom simulation model are presented to illustrate the efficacy of the approach by comparing the performance with an adaptive timescale separation-based guidance and control design. | en_US |
| dc.identifier.citation | Adaptive, Integrated Guidance and Control Design for Line-of-Sight-Based Formation Flight. Byoung S. Kim, Anthony J. Calise, Ramachandra J. Sattigeri. Journal of Guidance Control and Dynamics, 30(5):13, October, 2007. | en_US |
| dc.identifier.issn | 0731-5090 | |
| dc.identifier.uri | http://hdl.handle.net/1853/35892 | |
| dc.language.iso | en_US | en_US |
| dc.publisher | Georgia Institute of Technology | en_US |
| dc.publisher.original | American Institute of Aeronautics and Astronautics, Inc. | |
| dc.subject | Unmanned aerial vehicles | en_US |
| dc.subject | Adaptive control | en_US |
| dc.subject | Formation flight | en_US |
| dc.subject | Integrated guidance and control | en_US |
| dc.title | Adaptive, Integrated Guidance and Control Design for Line-of-Sight-Based Formation Flight | en_US |
| dc.type | Text | |
| dc.type.genre | Article | |
| dspace.entity.type | Publication | |
| local.contributor.corporatename | Daniel Guggenheim School of Aerospace Engineering | |
| local.contributor.corporatename | Aerospace Design Group | |
| local.contributor.corporatename | College of Engineering | |
| relation.isOrgUnitOfPublication | a348b767-ea7e-4789-af1f-1f1d5925fb65 | |
| relation.isOrgUnitOfPublication | a3341b9f-ecbe-4107-8198-7cfe1d286a80 | |
| relation.isOrgUnitOfPublication | 7c022d60-21d5-497c-b552-95e489a06569 |