Year |
Citation |
Score |
2016 |
Cano A, Sobel K. Simple Adaptive Delta Operator Aircraft Flight Control for Accommodation of Loss of Control Effectiveness Engineering. 8: 173-195. DOI: 10.4236/Eng.2016.84016 |
0.625 |
|
2014 |
Nieto-Wire C, Sobel K. Delta Operator Eigenstructure Assignment for Reconfigurable Control of a Tailless Aircraft Journal of Guidance Control and Dynamics. 37: 1824-1839. DOI: 10.2514/1.G000036 |
0.506 |
|
2011 |
Nieto-Wire C, Sobel K. Flight Control Design for a Tailless Aircraft Using Eigenstructure Assignment International Journal of Aerospace Engineering. 2011: 1-13. DOI: 10.1155/2011/549131 |
0.512 |
|
2007 |
Belkharraz AI, Sobel K. Simple adaptive control for aircraft control surface failures Ieee Transactions On Aerospace and Electronic Systems. 43: 600-611. DOI: 10.1109/Taes.2007.4285356 |
0.553 |
|
1996 |
Su W, Sobel K. CGT Adaptive Control of Non-ASPR Plants with Nonlinearities of Known Form Ifac Proceedings Volumes. 29: 5298-5303. DOI: 10.1016/S1474-6670(17)58523-7 |
0.383 |
|
1995 |
Piou JE, Sobel KM. Robust Multirate Eigenstructure Assignment with Flight Control Application Journal of Guidance Control and Dynamics. 18: 539-546. DOI: 10.2514/3.21420 |
0.559 |
|
1994 |
Piou JE, Sobel KM, Shapiro EY. Multirate eigenstructure assignment with application to an aircraft lateral SAS/autopilot Proceedings of the American Control Conference. 3: 2496-2500. |
0.454 |
|
1993 |
Piou JE, Sobel KM. Robust Sampled Data Eigenstructure Assignment Using the Delta Operator Journal of Guidance Control and Dynamics. 16: 702-711. DOI: 10.2514/3.21070 |
0.424 |
|
1993 |
Yu W, Piou JE, Sobel KM. Robust eigenstructure assignment for the extended medium range air-to-air missile Automatica. 29: 889-898. DOI: 10.1016/0005-1098(93)90094-A |
0.376 |
|
1992 |
Sobel KM, Yu W, Piou JE, Cloutier JR, Wilson R. Robust eigenstructure assignment with structured state-space uncertainty and unmodelled dynamics International Journal of Systems Science. 23: 765-788. DOI: 10.1080/00207729208949247 |
0.341 |
|
1992 |
Su W, Sobel KM. A unified theory for the CGT approach to adaptive control International Journal of Control. 56: 143-171. DOI: 10.1080/00207179208934307 |
0.414 |
|
1992 |
Sobel KM, Yu W. Robust Control Techniques for Systems with Structured State Space Uncertainty Control and Dynamic Systems. 51: 407-466. DOI: 10.1016/B978-0-12-012751-1.50015-X |
0.382 |
|
1991 |
Sobel KM, Yu W. Robust Eigenstructure Assignment with Structured State Space Uncertainty Journal of Guidance Control and Dynamics. 14: 621-628. DOI: 10.2514/3.20683 |
0.482 |
|
1991 |
Sobel KM, Yu W, Piou JE, Cloutier J, Wilson R. Robust eigenstructure assignment with structured state space uncertainty and unmodelled dynamics Proceedings of the American Control Conference. 3: 3137-3141. DOI: 10.1080/00207729208949247 |
0.444 |
|
1991 |
Yu W, Piou JE, Sobel KM. Robust eigenstructure assignment for the Extended Medium Range Air to Air Missile Proceedings of the Ieee Conference On Decision and Control. 3: 2976-2981. DOI: 10.1016/0005-1098(93)90094-A |
0.462 |
|
1990 |
Sobel KM, Lallman FJ, Yu W. Eigenstructure assignment with gain suppression using eigenvalue and eigenvector derivatives Journal of Guidance Control and Dynamics. 13: 1008-1013. DOI: 10.2514/3.20573 |
0.44 |
|
1990 |
Sobel KM, Piou JE, Yu W, Shapiro EY, Wilson R. A time approach to robustness of LTI systems with structured uncertainty and unmodelled dynamics Proceedings of the Ieee Conference On Decision and Control. 2: 432-433. |
0.359 |
|
1989 |
Sobel KM, Banda SS. Design of a modalized observer with eigenvalue sensitivity reduction Journal of Guidance Control and Dynamics. 12: 762-764. DOI: 10.2514/3.20476 |
0.319 |
|
1989 |
Sobel KM, Lallman FJ. Eigenstructure assignment for the control of highly augmented aircraft Journal of Guidance Control and Dynamics. 12: 318-324. DOI: 10.2514/3.20411 |
0.538 |
|
1989 |
Sobel KM, Banda SS, Yeh HH. Robust control for linear systems with structured state space uncertainty International Journal of Control. 50: 1991-2004. DOI: 10.1080/00207178908953478 |
0.433 |
|
1989 |
Sobel KM, Yu W, Shapiro EY. Systematic approach to gain suppression using eigenstructure assignment . 1292-1294. |
0.397 |
|
1987 |
Sobel KM, Shapiro EY. Application of Eigenstructure Assignment to Flight Control Design: Some Extensions Journal of Guidance Control and Dynamics. 10: 73-81. DOI: 10.2514/3.20183 |
0.445 |
|
1987 |
Sobel KM, Shapiro EY. FLIGHT CONTROL EXAMPLES OF ROBUST EIGENSTRUCTURE ASSIGNMENT Proceedings of the Ieee Conference On Decision and Control. 1290-1291. |
0.413 |
|
1987 |
Sobel KM, Shapiro EY. ROBUSTNESS/PERFORMANCE TRADEOFFS IN EIGENSTRUCTURE ASSIGNMENT WITH FLIGHT CONTROL APPLICATION Proceedings of the American Control Conference. 380-385. |
0.341 |
|
1986 |
Sobel KM, Kaufman H. Direct Model Reference Adaptive Control for a Class of MIMO Systems Control and Dynamic Systems. 24: 245-314. DOI: 10.1016/B978-0-12-012724-5.50008-3 |
0.446 |
|
1986 |
Sobel KM, Lee HP, Ioannou P. APPLICATION OF ROBUST DIRECT ADAPTIVE CONTROL TO THE LONGITUDINAL DYNAMICS OF A FIGHTER AIRCRAFT Proceedings of the Ieee Conference On Decision and Control. 844-845. |
0.47 |
|
1986 |
Sobel KM, Shapiro EY. FLIGHT CONTROL SYNTHESIS VIA EIGENSTRUCTURE ASSIGNMENT. THE DISCRETE VERSION . 1-6. |
0.433 |
|
1986 |
Sobel KM, Shapiro EY. DESIGN OF DYNAMIC COMPENSATORS VIA EIGENSTRUCTURE ASSIGNMENT WITH FLIGHT CONTROL APPLICATIONS Ieee Proceedings of the National Aerospace and Electronics Conference. 408-414. |
0.334 |
|
1985 |
Shapiro EY, Sobel KM. Eigenstructure Assignment for Design of Multimode Flight Control Systems Ieee Control Systems Magazine. 5: 9-15. DOI: 10.1109/MCS.1985.1104941 |
0.395 |
|
1985 |
Sobel KM, Shapiro EY. EIGENSTRUCTURE ASSIGNMENT, EIGENSENSITIVITY, AND FLIGHT CONTROL DESIGN Proceedings of the Ieee Conference On Decision and Control. 658-659. |
0.374 |
|
1985 |
Sobel KM, Shapiro EY. EIGENSTRUCTURE ASSIGNMENT: A TUTORIAL - PART II APPLICATIONS Proceedings of the American Control Conference. 461-467. |
0.46 |
|
1984 |
Sobel KM, Shapiro EY, Rooney RH. SYNTHESIS OF DIRECT LIFT CONTROL LAWS VIA EIGENSTRUCTURE ASSIGNMENT Ieee Proceedings of the National Aerospace and Electronics Conference. 1: 570-575. |
0.322 |
|
1984 |
Sobel KM, Shapiro EY. APPLICATION OF EIGENSYSTEM ASSIGNMENT TO LATERAL TRANSLATION AND YAW POINTING FLIGHT CONTROL Proceedings of the Ieee Conference On Decision and Control. 1423-1428. |
0.453 |
|
1983 |
Sobel KM, Chung JC, Shapiro EY. APPLICATION OF MIMO PHASE AND GAIN MARGINS TO THE EVALUATION OF A FLIGHT CONTROL SYSTEM Proceedings of the American Control Conference. 3: 1286-1287. |
0.332 |
|
1983 |
Sobel KM, Shapiro EY. ROBUST PITCH POINTING CONTROL LAW Proceedings of the Ieee Conference On Decision and Control. 3: 1088-1093. |
0.392 |
|
1983 |
Sobel KM, Shapiro EY. DESIGN METHODOLOGY FOR PITCH POINTING FLIGHT CONTROL SYSTEMS USING EIGENSTRUCTURE ASSIGNMENT . 635-640. |
0.393 |
|
1982 |
Sobel KM. MODEL REFERENCE ADAPTIVE CONTROL FOR A RELAXED STATE STABILITY AIRCRAFT Proceedings of the Ieee Conference On Decision and Control. 3: 1369-1373. |
0.335 |
|
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