This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
The Feasibility of Using an INS for Control System Feedbacks
Annotation ability available
Sector:
Language:
English
Abstract
It has been suggested that the conventional air data probes used on modern high performance aircraft can be eliminated by exploiting the capabilities of the Inertial Navigation System (INS) and obtaining analytic estimates of angle-of-attack (α), sideslip angle (β), and possibly of dynamic pressure (q). The reasons for wanting to eliminate the probes are that they are vulnerable to ground handling damage, bird strikes, icing, and hostile action in the case of combat aircraft. To determine the feasibility of this approach, three methods for obtaining α and β estimates from INS information were programmed into a nonlinear simulation of a relaxed stability aircraft which requires a high level of artificial stability augmentation through its flight control system. It was found that none of the three methods provided satisfactory stabilizing feedbacks to the control system when the subject aircraft was disturbed by severe atmospheric turbulence. This was due to the inability of the INS to determine the airframe orientation relative to the motion of the atmosphere. Simulation results for each of the three methods were compared with the results obtained when conventional probes were used to obtain direct measurements of α and β. An alternate method for determining α and β analytically that would be satisfactory for use in turbulence is presented.
Recommended Content
Journal Article | A Robust Physical Layer for Aircraft Data Networks Based on MIL-STD-1553 |
Technical Paper | X-29A Subsystems Integration - An Example for Future Aircraft |
Aerospace Standard | PRIMARY FLIGHT CONTROLS BY ELECTRICAL SIGNALING SECTION I |
Authors
Citation
Colgren, R., "The Feasibility of Using an INS for Control System Feedbacks," SAE Technical Paper 985517, 1998, https://doi.org/10.4271/985517.Also In
References
- Colgren, Richard “Nonlinear H ∞ Control of a Missile's Roll Axis,” Proceedings of the 1994 American Control Conference Baltimore, MD 2 3 2109 2113 29 June 1 July 1994
- Colgren, Richard “H ∞ Design of Future Flight Control Systems,” Proceedings of the Fifth IEEE International Symposium on Intelligent Control Philadelphia, Pennsylvania 2 2 805 810 5-7 September 1990
- Colgren, Richard “Workstation for the Integrated Design and Simulation of Flight Control Systems,” Control Systems Magazine 9 4 25 28 June 1989
- Etkin, Bernard “Dynamics of Atmospheric Flight,” John Wiley & Sons, Inc. New York, New York 1972
- McRuer, Duane Ashkenas, Irving Graham, Dunstan “Aircraft Dynamics and Automatic Control,” Princeton University Press Princeton, New Jersey 1973