Aeronautical Engineering

Fault-tolerant flight control and guidance systems: by Guillaume J. J. Ducard

By Guillaume J. J. Ducard

Unmanned aerial cars (UAVs) provide an incomparable technique of amassing intelligence and engaging in missions with no need an onboard human pilot. the advantages are substantial when it comes to rate, potency, and lowered pilot risk.

In order to accomplish a venture successfully and with a excessive point of security and safety, the subsequent key layout issues needs to be met:

• the flight keep an eye on method has to be powerful opposed to the aircraft’s version uncertainties and exterior disturbances;

• an effective fault detection and isolation (FDI) procedure might be in a position to tracking the wellbeing and fitness of the plane; and

• the flight keep an eye on and assistance procedure can be reconfigurable reckoning on actuator fault incidence or plane harm, and may manage to keep away from obstacles.

Fault-tolerant Flight regulate and assistance Systems addresses all of those points with a realistic technique following 3 major requisites: being appropriate in real-time; hugely computationally effective; and modular. The textual content provides:

• an outline of fault-tolerant flight keep an eye on techniques;

• the required equations for the modeling of small UAVs;

• an entire nonlinear FDI process in response to prolonged Kalman filters; and

• a nonlinear flight keep watch over and assistance system.

The publication is written in a didactic sort with many figures and diagrams making it compatible not just for educational researchers and practising engineers but in addition graduate scholars operating within the fields of fault detection innovations and the automated keep an eye on of UAVs.

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In AIAA Guidance, Navigation, and Control Conference and Exhibit, Keystone, CO, 2006. 68. D. Enns. Robustness of Dynamic Inversion vs. μ Synthesis: Lateral Directional Flight Control Example. AIAA paper 90-3338-CP, 1990. 69. M. G. Goman and E. N. Kolesnikov. Robust Nonlinear Dynamic Inversion Method for an Aircraft Motion Control. Paper AIAA-98-4208, pp. 511−521, 1998. 70. M. B. McFarland and S. M. Hoque. Robustness of a Nonlinear Missile Autopilot Designed Using Dynamic Inversion. In Proceedings of AIAA Guidance, Navigation, and Control Conference and Exhibit, Denver, CO, 14−17 August 2000.

Keviczky, and G. J. Balas. Fault-Detection Design for Unhinhabited Aerial Vehicles. AIAA Journal of Guidance, Control, and Dynamics, 29(5):1051–1060, September-October 2006. 53. R. J. Patton, P. M. Frank, and R. N. Clark. Issues of Fault Diagnosis for Dynamic Systems. Springer-Verlag, London, 2000. 54. R. J. Patton, F. J. Uppal, S. Simani, and B. Polle. Reliable Fault Diagnosis Scheme for a Spacecraft Control System. Journal of Risk and Reliability, 222:139–152, 2008. 1243/1748006XJRR98. 22 2 Review 55.

AIAA Journal of Guidance, Control, and Dynamics, 26(5):719–727, 2003. 85. K. A. Wise, E. Lavretsky, and N. Hovakimyan. Adaptive Control of Flight: Theory, Applications, and Open Problems. In Proceedings of the IEEE American Control Conference, pages 5966–5971, Minneapolis, MN, June 2006. 86. C. I. Ahn, Y. Kim, and H. J. Kim. Adaptive Sliding Mode Controller Design for Fault Tolerant Flight Control System. In Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, Keystone, CO, August 2006.

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