Real-time optimal techniques for unmanned air vehicles fuel saving
Authors:
Open Access
- 29 November 2011
- journal article
- research article
- Published by SAGE Publications in Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
- Vol. 226 (10) , 1315-1328
Abstract
Dynamic soaring can save fuel by the extraction of low-altitude wind shear energy. The problem of generating energy-saving trajectories in real time for an unmanned powered sailplane is considered. A method called ‘inverse dynamics in the virtual domain’ is investigated. The method results in rapid solution generation and is suitable for real-time applications. Three-dimensional unmanned aerial vehicle equations of motion and a non-linear wind gradientmodel are used. Trajectories are generated to minimize the total power used per horizontal distance travelled for cross-wind travelling and in the total power used per total time in air for loitering mode. Trajectory following issues are addressed and an architecture for the control system is briefly described. A method for the estimation of wind shear gradient parameters is proposed. Validation is performed using a full six-degree-of-freedom model of a powered sailplane to verify the trajectory generation method.Keywords
This publication has 17 references indexed in Scilit:
- Engineless Unmanned Aerial Vehicle Propulsion by Dynamic SoaringJournal of Guidance, Control, and Dynamics, 2009
- Improved Endurance of Optimal Periodic FlightJournal of Guidance, Control, and Dynamics, 2007
- Minimum fuel powered dynamic soaring of unmanned aerial vehicles utilizing wind gradientsOptimal Control Applications and Methods, 2004
- Optimal patterns of glider dynamic soaringOptimal Control Applications and Methods, 2004
- Direct Method for Rapid Prototyping of Near-Optimal Aircraft TrajectoriesJournal of Guidance, Control, and Dynamics, 2000
- Periodic optimal flightJournal of Guidance, Control, and Dynamics, 1996
- Reducing fuel consumption of subsonic aircraft by optimal cyclic cruiseJournal of Aircraft, 1987
- Endurance increase by cyclic controlJournal of Guidance, Control, and Dynamics, 1986
- Nonoptimality of the steady-state cruise for aircraftAIAA Journal, 1976
- On the Fuel Optimality of CruiseJournal of Aircraft, 1973