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A frequency domain stability analysis of a phase plane control system
1985
Journal of Guidance Control and Dynamics
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A frequency domain stability analysis of the closed-loop control system is applied to a study of potential flight control system interaction with the Orbiter and a class of payloads deployed from a tilt ...
In application of the technique to stabil- ity analysis of the on-orbit Reaction Control System during deployment of a class of payloads using tilt tables, good agreement was shown between the describing ...
doi:10.2514/3.19934
fatcat:3cbsqeeqerhr5pvimirpxso63q
Subject Index 1985
1985
Journal of Guidance Control and Dynamics
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of Multivariable Feedback Systems G85-029 The Number of Multiplications Required to Chain Coordinate Transformations G85-027 A Frequency Domain Stability Analysis of a Phase Plane Control System G85-008 ...
of Payload Motions on the Nuta- tional Stability of the Galileo Spacecraft G8S-118 Characteristic Elastic Systems of Time-Lim- ited Optimal Maneuvers G85-108 Low Earth Orbit Navigation in the Tracking ...
doi:10.2514/3.56398
fatcat:fwii4heznza5dmx2qoovxklu5y
Using ergodicity of chaotic systems for improving the global properties of the delayed feedback control method
2009
Physical Review E
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To evaluate the closeness of the system state to the target orbit, a special algorithm is devised. For continuous-time systems, it can be implemented by means of a simple low-pass filter. ...
We do not perturb the system until its state approaches a desired unstable periodic orbit and then we activate the delayed feedback control force. ...
The analysis of global properties of DFC systems, such as basins of attraction of stabilized orbits, is much more complicated problem. ...
doi:10.1103/physreve.80.067201
pmid:20365303
fatcat:mwpkxehm4jfbhg65dramn3gk3y
Libration Control of Electrodynamic Tethers Using the Extended Time-Delayed Autosynchronization Method
2010
Journal of Guidance Control and Dynamics
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Such a stabilized periodic orbit can be taken as the starting point for the operation of the electrodynamic tether. ...
This analysis assumes a rigid tether, with two end masses orbiting along a circular inclined orbit, and a constant tether current, which does not depend on the attitude and orbital position of the tether ...
Acknowledgments The work of M. Iñarrea is part of the research project MTM2008-03818. The work of J. Peláez was carried out under the research project ESP2007-64068. ...
doi:10.2514/1.44232
fatcat:ibn5mvmngndt3lxareiy3jqbdy
Bifurcation analysis of the attitude dynamics for a magnetically controlled spacecraft
2012
2012 IEEE 51st IEEE Conference on Decision and Control (CDC)
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Bifurcation analysis of controlled spacecraft model Outline • Spacecraft models and magnetic control • Local stability analysis • Bifurcation analysis • Simulation results • Concluding remarks and future ...
works 2 Bifurcation analysis of controlled spacecraft model ...
Local stability analysis First approach: analyze the local stability of the (q,ω)=([0 0 0 1] T ,0) equilibrium of the closed loop periodically forced system. ...
doi:10.1109/cdc.2012.6426150
dblp:conf/cdc/RossaBL12
fatcat:3n2q4qpgqnhlrf6nq623nyb6xa
Floquet stability analysis of Ott–Grebogi–Yorke and difference control
2008
New Journal of Physics
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2008 accepted arXiv:nlin/0204060v3 fatcat:d567u3qlzncrnbqt2kwwbherwaOther Versions
Stabilization of instable periodic orbits of nonlinear dynamical systems has been a widely explored field theoretically and in applications. ...
Here a new stability analysis of these two Poincar\'e-based chaos control schemes is given by means of Floquet theory. ...
Acknowledgments The author acknowledges financial support from Deutsche Forschungsgemeinschaft (DFG) through SFB-654 "Plasticity and Sleep". ...
doi:10.1088/1367-2630/10/6/063006
fatcat:7m5o4jk6xrachpdf7hlyvrakly
Continuous-time controllers for stabilizing periodic orbits of hybrid systems: Application to an underactuated 3D bipedal robot
2014
53rd IEEE Conference on Decision and Control
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This paper presents a systematic approach to exponentially stabilize periodic orbits in nonlinear systems with impulse effects, a special class of hybrid systems. ...
By investigating the properties of the Poincaré return map, a sensitivity analysis is presented that translates the stabilization problem into a set of Bilinear Matrix Inequalities (BMIs). ...
On the basis of the sensitivity analysis, the problem of stabilization of the periodic orbits is then translated into a set of bilinear matrix inequalities. ...
doi:10.1109/cdc.2014.7039613
dblp:conf/cdc/HamedBG14
fatcat:jbhxtl2hrjd4pdmua5dh2bnc6e
Book Announcements
1992
Journal of Guidance Control and Dynamics
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F., On-Orbit Servicing of Space Systems, Krieger, Melbourne, FL, 1992.
Purpose: This book presents the past, present, and future of orbital servicing. ...
Purpose: This reference stresses the latest geometric meth- ods for multivariable control system analysis and design. ...
doi:10.2514/3.56571
fatcat:lbv7l22rxfei3kguwhlu5hawie
Libration Control of Electrodynamic Tethers in Inclined Orbit
2005
Journal of Guidance Control and Dynamics
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the control forces needed to stabilize the system with the second control law. ...
Therefore, we will analyze first the stability properties of this simplified control scheme. Then we will use the results of this analysis to check the TDAS control scheme. ...
doi:10.2514/1.6473
fatcat:ayhcyllbv5aj7af3c5nqmw3duu
Evolutionary Synthesis and Control of Chaotic Systems
2009
IFAC Proceedings Volumes
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new cost functions operating in "blackbox mode" without previous exact mathematical analysis of the system, thus without knowledge of stabilizing of the target state. ...
The main aim of this work is to show that evolutionary algorithms are capable of synthesis of new chaotic system and optimization of its control and to show a new approach of solving this problem and constructing ...
Control of chaos, p-1 orbit, CF 1 The first case is focused on the stabilization of p-1 orbit. Unperturbed chaotic system has this p-1 orbit: x F = -1.0772 (A = 1.15). ...
doi:10.3182/20090622-3-uk-3004.00057
fatcat:dnzalc5scffyhhehs523ez2rky
Can we make a robot ballerina perform a pirouette? Orbital stabilization of periodic motions of underactuated mechanical systems
2008
Annual Reviews in Control
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orbitally stabilizing control designs. ...
When studying the orbital stabilization of periodic motions of underactuated mechanical sys- ...
The local exponential stabilization task (see Problem 3 above) in the case when the desired orbit is just an equilibrium can be approached via analysis of the standard controlled linearization: z =Āz + ...
doi:10.1016/j.arcontrol.2008.07.001
fatcat:eq4echhcsbguxc45tfta6q3vgi
CAN WE MAKE A ROBOT BALLERINA PERFORM A PIROUETTE? ORBITAL STABILIZATION OF PERIODIC MOTIONS OF UNDERACTUATED MECHANICAL SYSTEMS1
2007
IFAC Proceedings Volumes
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orbitally stabilizing control designs. ...
When studying the orbital stabilization of periodic motions of underactuated mechanical sys- ...
The local exponential stabilization task (see Problem 3 above) in the case when the desired orbit is just an equilibrium can be approached via analysis of the standard controlled linearization: z =Āz + ...
doi:10.3182/20070829-3-ru-4911.00005
fatcat:oza3u6ctxfcrdg6lsbvgib4ucu
Subject Index
2011
Journal of Guidance Control and Dynamics
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- lope Protection Systems for Small Aircraft G11-105 Stability Properties and Cross-Coupling Performance of the Control Allocation Scheme CAPIO
G11-085 Fault-Tolerant Attitude Control for Spacecraft Under ...
Control of Clustered Electrodynamic Tether System Using Kuramoto Model
G11-139 Linear Parameter Varying Analysis of Switched Controllers for Attitude Control Systems
G11-174 Modified Singular-Direction ...
doi:10.2514/1.56394
fatcat:h2hs6frx4fhmfmklgp5pzdavdy
Control System Design Technique and Validation for A High-Resolution Mapping Satellite
2021
E3S Web of Conferences
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Based on the author's multi-year research on the design of high-resolution satellite control system, the key technologies and design methods for the high-precision attitude measurement and control system ...
Since China's first satellite measuring scale of 1:10,000 was launched in 2019, thus GF-7 satellite has realized the arc-second attitude measurement accuracy, where the degree of stability reached 10- ...
Through the analysis of in-orbit remote sensing data, the control system reached the indexes as required. ...
doi:10.1051/e3sconf/202123304041
fatcat:x7ou3q4saffbrpoqzfokhz6744
A Twenty-Year Review of Time-Delay Feedback Control and Recent Developments
2014
IEICE Proceeding Series
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The method allows a noninvasive stabilization of UPOs of dynamical systems in the sense that the control force vanishes when the target state is reached. ...
Note that only the stability properties of the orbit are changed, while the orbit itself and its period remain unaltered. ...
Even linear analysis of such systems is complicated due to the infinite number of Floquet exponents characterizing the stability of controlled orbits. ...
doi:10.15248/proc.1.683
fatcat:inzq2u4m4zhlpli33lyeyhmhju
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