TY - GEN
T1 - H ∞ tracking with commands generated by unstable autonomous systems having initial conditions in finite hyper-rectangles
AU - Boyarski, S.
AU - Yaesh, I.
AU - Shaked, U.
PY - 2010
Y1 - 2010
N2 - This paper presents a novel approach to H ∞ analysis of tracking problems, where the command signal is generated by a possibly unstable autonomous generating system (AGS), whose dynamics corresponds to the practically expected commands and whose output results only from its initial conditions (ICs). An unstable AGS (e.g. double integrator) allows generation of realistic, common command-signals that cannot be created by standard shaping filters acting on white noise or on finite-energy signals. The analysis addresses linear time-invariant possibly unstable systems in a finite-horizon setting. The unknown ICs of both the system and the AGS are assumed to lie in finite hyper-rectangles, analogously to the standard treatment of parameter-uncertainty. It is shown that the dependence of the system's performance on such ICs is convex; this fact leads to theorems assuring a H ∞ performance bound over the two ICs uncertainty regions (jointly). A solution to an 'inverse problem', i.e. finding the maximum-volume ICs hyper-rectangles for a given performance level, is also presented. The example addresses an aircraft responding to a variety of mixed step and ramp vertical acceleration commands.
AB - This paper presents a novel approach to H ∞ analysis of tracking problems, where the command signal is generated by a possibly unstable autonomous generating system (AGS), whose dynamics corresponds to the practically expected commands and whose output results only from its initial conditions (ICs). An unstable AGS (e.g. double integrator) allows generation of realistic, common command-signals that cannot be created by standard shaping filters acting on white noise or on finite-energy signals. The analysis addresses linear time-invariant possibly unstable systems in a finite-horizon setting. The unknown ICs of both the system and the AGS are assumed to lie in finite hyper-rectangles, analogously to the standard treatment of parameter-uncertainty. It is shown that the dependence of the system's performance on such ICs is convex; this fact leads to theorems assuring a H ∞ performance bound over the two ICs uncertainty regions (jointly). A solution to an 'inverse problem', i.e. finding the maximum-volume ICs hyper-rectangles for a given performance level, is also presented. The example addresses an aircraft responding to a variety of mixed step and ramp vertical acceleration commands.
UR - http://www.scopus.com/inward/record.url?scp=84867785904&partnerID=8YFLogxK
U2 - 10.2514/6.2010-8410
DO - 10.2514/6.2010-8410
M3 - ???researchoutput.researchoutputtypes.contributiontobookanthology.conference???
AN - SCOPUS:84867785904
SN - 9781600869624
T3 - AIAA Guidance, Navigation, and Control Conference
BT - AIAA Guidance, Navigation, and Control Conference
T2 - AIAA Guidance, Navigation, and Control Conference
Y2 - 2 August 2010 through 5 August 2010
ER -