Title :
Resource balancing control allocation
Author :
Frost, S.A. ; Bodson, M.
Author_Institution :
NASA Ames Res. Center, Moffett Field, CA, USA
fDate :
June 30 2010-July 2 2010
Abstract :
Next generation aircraft with a large number of actuators will require advanced control allocation methods to compute the actuator commands needed to follow desired trajectories while respecting system constraints. Previously, algorithms were proposed to minimize the l1 or l2 norms of the tracking error and of the control effort. The paper discusses the alternative choice of using the l1 norm for minimization of the tracking error and a normalized l221E; norm, or sup norm, for minimization of the control effort. The algorithm computes the norm of the actuator deflections scaled by the actuator limits. Minimization of the control effort then translates into the minimization of the maximum actuator deflection as a percentage of its range of motion. The paper shows how the problem can be solved effectively by converting it into a linear program and solving it using a simplex algorithm. Properties of the algorithm are investigated through examples. In particular, the min-max criterion results in a type of resource balancing, where the resources are the control surfaces and the algorithm balances these resources to achieve the desired command. A study of the sensitivity of the algorithms to the data is presented, which shows that the normalized l221E; algorithm has the lowest sensitivity, although high sensitivities are observed whenever the limits of performance are reached.
Keywords :
actuators; distributed control; optimisation; position control; actuator commands; actuator deflections; linear program; resource balancing control allocation; tracking error; Actuators; Aerospace control; Aircraft propulsion; Control systems; Error correction; Linear programming; Resource management; Testing; USA Councils; Vehicles;
Conference_Titel :
American Control Conference (ACC), 2010
Conference_Location :
Baltimore, MD
Print_ISBN :
978-1-4244-7426-4
DOI :
10.1109/ACC.2010.5530448