in:(KONSTANTIN KONDAK)

SYSTEM FOR CONTROLLING ROTARY-WING UNMANNED AIRCRAFT FOR VERTICAL LANDING ON MOVING SURFACES BY FEEDING FORWARD FORCES IN THE CONTROL SYSTEM ES201232073A
[KONDAK KONSTANTIN, BEJAR DOMINGUEZ MANUEL, OLLERO BATURONE ANIBAL, SANDINO VELASQUEZ LUIS ALBERTO, SANTAMARIA RUBIO DANIEL, JIMENEZ BELLIDO ANTONIO, ALARCON ROMERO FRANCISCO, VIGURIA JIMENEZ LUIS ANTIDIO, ALBO SANCHEZ-BEDOYA CARLOS, ANDERSON BELL SEILER ALLAN, GIL MONTANO PABLO, DE LOS SANTOS TRIGO SILVIA] ES;ES;ES;DE The invention relates to an improvement to the control system for landing a VTOL unmanned aircraft on a moving platform, comprising the addition of: a sensor-based control system, said sensors measuring the tension of the cable that connects the aircraft to the landing platform and the angles of orientation of said cable with respect to a system connected to the aircraft and a control module that receives as input the tension - both in terms of magnitude and direction - obtained from the sensors, as well as the control settings generated by the aircraft controller. Based on the tension in the cable, the control module of the invention calculates corrections to be incorporated into the control settings, which anticipate the disruptions that will occur to the position of the aircraft as a consequence of the changes in the tension of the cable.
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SYSTEM FOR CONTROLLING ROTARY-WING UNMANNED AIRCRAFT FOR VERTICAL LANDING ON MOVING SURFACES BY FEEDING FORWARD FORCES IN THE CONTROL SYSTEM PCT/ES2013/070935
[KONDAK, Konstantin] Ctra. De Utrera, Km.1 E-41013 Sevilla;Pabellon De Brasil, Paseo De Las Delicias, S/N E-41013 Sevilla;Wilbur Y Orvilla Wright, 13 E-41309 La Rinconada-Sevilla;Uhlandstr, 3 10623 Berlin The invention relates to an improvement to the control system for landing a VTOL unmanned aircraft on a moving platform, comprising the addition of: a sensor-based control system, said sensors measuring the tension of the cable that connects the aircraft to the landing platform and the angles of orientation of said cable with respect to a system connected to the aircraft; and a control module that receives as input the tension — both in terms of magnitude and direction — obtained from the sensors, as well as the control settings generated by the aircraft controller. Based on the tension in the cable, the control module of the invention calculates corrections to be incorporated into the control settings, which anticipate the disruptions that will occur to the position of the aircraft as a consequence of the changes in the tension of the cable.
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DE102018120844A
[KONDAK KONSTANTIN, OTT CHRISTIAN, JUN KIM MIN, SARKISOV IURII, GRUNERT LINUS] DE
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DEVICE FOR INFLUENCING MOVEMENT WITH A PARALLEL MECHANISM PCT/DE2003/002763
[KONDAK, Konstantin, HOMMEL, Günter] Strasse des 17. Juni 135 10623 Berlin;Uhlandstrasse 3 10623 Berlin;Friedbergstrasse 3 14057 Berlin The invention relates to a device for influencing a movement of body parts of a living being, comprising a base for placing on a body part of a living being and a platform for placing on another body part of the living being, whereby the base and the platform can be moved relative to one another. The base and the platform are connected to one another by means of a number of actuators whereby forming a parallel mechanism.
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DE102018120844A
[KONDAK KONSTANTIN, OTT CHRISTIAN, JUN KIM MIN, SARKISOV IURII, GRUNERT LINUS] DE
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DE10238256A
[KONDAK KONSTANTIN] DE
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ES201232073A
[KONDAK KONSTANTIN, BEJAR DOMINGUEZ MANUEL, OLLERO BATURONE ANIBAL, SANDINO VELASQUEZ LUIS ALBERTO, SANTAMARIA RUBIO DANIEL, JIMENEZ BELLIDO ANTONIO, ALARCON ROMERO FRANCISCO, VIGURIA JIMENEZ LUIS ANTIDIO, ALBO SANCHEZ-BEDOYA CARLOS, ANDERSON BELL SEILER ALLAN, GIL MONTANO PABLO, DE LOS SANTOS TRIGO SILVIA] ES;ES;ES;DE
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DE102020129956A
[VILZMANN MICHAEL, KONDAK KONSTANTIN, SHAIKH KHIZER] DE
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Control system of unmanned rotary wing aircraft for vertical landing on moving surfaces by pre-feeding forces in the control system, perfected (Machine-translation by Google Translate, not legally binding) ES201431792A
[KONSTANTIN KONDAK, BEJAR DOMINGUEZ MANUEL, SANDINO VELAZQUEZ LUIS ALBERTO, SANTAMARIA RUBIO DANIEL, JIMENEZ BELLIDO ANTONIO, ALARCON ROMERO FRANCISCO, VIGURIA JIMENEZ LUIS ANTIDIO, BELL SEILER ALLAN ANDERSON] ES;ES;ES;DE Addition to the main patent p201232073 based on the incorporation of a control system, consisting of sensors, which measure the tension of the cable that connects the aircraft with the landing platform and the angles of orientation of said cable with respect to an associated system to the aircraft, and a control module that takes as inputs the voltage -both in magnitude and in direction- obtained from the mentioned sensors, in addition to the control slogans generated by the aircraft controller. The control module object of the invention calculates, from the tension in the cable, corrections to be entered in the control instructions. (Machine-translation by Google Translate, not legally binding)
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ES201431792A
[KONSTANTIN KONDAK, BEJAR DOMINGUEZ MANUEL, SANDINO VELAZQUEZ LUIS ALBERTO, SANTAMARIA RUBIO DANIEL, JIMENEZ BELLIDO ANTONIO, ALARCON ROMERO FRANCISCO, VIGURIA JIMENEZ LUIS ANTIDIO, BELL SEILER ALLAN ANDERSON] ES;ES;ES;DE
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