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Institution

Spar Aerospace

About: Spar Aerospace is a based out in . It is known for research contribution in the topics: Antenna (radio) & Communications satellite. The organization has 272 authors who have published 252 publications receiving 3186 citations. The organization is also known as: Special Products/Applied Research.


Papers
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Patent
22 May 1989
TL;DR: In a human-in-the-loop robotic control loop, the constrained forces and moments at the gripper (also called hand or end effector) of the manipulator are measured by a force-mement sensor as mentioned in this paper.
Abstract: In a human-in-the-loop robotic control loop, the constrained forces and moments at the gripper (also called hand or end effector) of the manipulator are measured by a force-mement sensor. The resulting force and moment signals are scaled and fed as input voltages to motors in a hand controller to provide torques which oppose deflection of the hand controller. Thus, the operator feels the opposing torques which are proportional to the magnitude of the constrained forces and moments. The force feedback loop may be opened to selectively provide a passive control loop. In either the active or passive mode, the hand controller position signals may be selectively mapped to either gripper position signals or gripper velocity signals in order to control movement of the gripper in the desired manner.

200 citations

Journal ArticleDOI
TL;DR: In this article, a novel adaptive filtering technique is described for a class of systems with unknown disturbances, which includes both a self-tuning filter and a Kalman filter, and state estimates are employed in a closed-loop feedback control scheme which is designed via the usual linear quadratic approach.
Abstract: A novel adaptive filtering technique is described for a class of systems with unknown disturbances. The estimator includes both a self-tuning filter and a Kalman filter. The state estimates are employed in a closed-loop feedback control scheme which is designed via the usual linear quadratic approach. The approach was developed for application to the dynamic ship positioning control problem and has the advantage that existing nonadaptive Kalman filtering systems may be easily modified to include the self-tuning feature.

144 citations

Patent
24 Jun 1996
TL;DR: In this paper, a satellite data communication system and method of operating the same is disclosed, where access schemes, protocols and switching techniques are combined to offer optimized dynamic bandwidth-on-demand on a cell-by-cell basis.
Abstract: A satellite data communication system and method of operating the same is disclosed. The satellite data communication system provides switched transport services for multi-media networks, wherein access schemes, protocols and switching techniques are combined to offer optimized dynamic bandwidth-on-demand on a cell-by-cell basis.

133 citations

Journal ArticleDOI
TL;DR: In this paper, the authors examined the properties of probing signals employed in a model reference identification procedure which guarantee identification of the parameters of a linear multivariable system, including persistent excitation.
Abstract: This paper examines certain properties of probing signals employed in a model reference identification procedure which guarantee identification of the parameters of a linear multivariable system. The property of persistent excitation is examined with respect to a new class of (persistently spanning) signals. In particular, this class of signals includes many (periodic or almost periodic) signals which have previously been considered as effective probing signals, The results yield concrete guidelines useful in the practical design of probing signals.

125 citations

Journal ArticleDOI
01 Jun 1991
TL;DR: Technical problems addressed include calibration, rapid data processing, the phased array antenna that provides controlled beam steering, and the first satellite implementation of a special radar technique known as ScanSAR.
Abstract: RADARSAT, the first Canadian remote-sensing spacecraft, is designed to provide Earth observation information for five years. The satellite is scheduled for launch in 1994. The only payload instrument is a 5.6-cm-wavelength (C-band) synthetic aperture imaging radar (SAR). RADARSAT will gather data on command for up to 28 min during each cycle of its 800-km (nominal) near-polar orbit. Image resolutions from 10 to 100 m at swath widths of 45 to 500 km will be available. The RADARSAT mission is reviewed, and the design, characteristics, and implementation of the radar are introduced. Technical problems addressed include calibration, rapid data processing, the phased array antenna that provides controlled beam steering, and the first satellite implementation of a special radar technique known as ScanSAR. >

123 citations


Authors

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Performance
Metrics
No. of papers from the Institution in previous years
YearPapers
20111
20091
20051
20041
19995
199811