BE478679A - - Google Patents
Info
- Publication number
- BE478679A BE478679A BE478679DA BE478679A BE 478679 A BE478679 A BE 478679A BE 478679D A BE478679D A BE 478679DA BE 478679 A BE478679 A BE 478679A
- Authority
- BE
- Belgium
- Prior art keywords
- signal
- control
- servo
- rudder
- rotor
- Prior art date
Links
- 238000004804 winding Methods 0.000 claims description 139
- 230000006698 induction Effects 0.000 claims description 56
- 230000033001 locomotion Effects 0.000 claims description 48
- 230000008878 coupling Effects 0.000 claims description 30
- 238000010168 coupling process Methods 0.000 claims description 30
- 238000005859 coupling reaction Methods 0.000 claims description 30
- 230000005284 excitation Effects 0.000 claims description 19
- 238000006073 displacement reaction Methods 0.000 claims description 15
- 230000009471 action Effects 0.000 claims description 13
- 230000001939 inductive effect Effects 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 3
- 230000004907 flux Effects 0.000 claims description 3
- 230000035945 sensitivity Effects 0.000 claims description 2
- 230000001360 synchronised effect Effects 0.000 claims description 2
- 230000007246 mechanism Effects 0.000 claims 2
- PWNAWOCHVWERAR-UHFFFAOYSA-N Flumetralin Chemical compound [O-][N+](=O)C=1C=C(C(F)(F)F)C=C([N+]([O-])=O)C=1N(CC)CC1=C(F)C=CC=C1Cl PWNAWOCHVWERAR-UHFFFAOYSA-N 0.000 claims 1
- 230000036541 health Effects 0.000 claims 1
- 102220024624 rs267607620 Human genes 0.000 claims 1
- 239000004020 conductor Substances 0.000 description 58
- 230000007935 neutral effect Effects 0.000 description 24
- 230000009467 reduction Effects 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 7
- 230000007423 decrease Effects 0.000 description 7
- 230000006978 adaptation Effects 0.000 description 6
- 230000008859 change Effects 0.000 description 5
- 230000010355 oscillation Effects 0.000 description 5
- 238000010276 construction Methods 0.000 description 4
- 238000013016 damping Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 229920006395 saturated elastomer Polymers 0.000 description 3
- 230000001133 acceleration Effects 0.000 description 2
- 238000013459 approach Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 239000003638 chemical reducing agent Substances 0.000 description 2
- 230000001627 detrimental effect Effects 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 241001580947 Adscita statices Species 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000036461 convulsion Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000010363 phase shift Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
- G05D1/085—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to ensure coordination between different movements
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Toys (AREA)
Publications (1)
Publication Number | Publication Date |
---|---|
BE478679A true BE478679A (enrdf_load_html_response) |
Family
ID=126374
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE478679D BE478679A (enrdf_load_html_response) |
Country Status (1)
Country | Link |
---|---|
BE (1) | BE478679A (enrdf_load_html_response) |
-
0
- BE BE478679D patent/BE478679A/fr unknown
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0435708B1 (fr) | Procédé de contrôle d'attitude en roulis et en lacet d'un satellite | |
US5259577A (en) | Attitude control system for three-axis stabilized satellite in near-equatorial orbit | |
EP3248079B1 (fr) | Procédé et dispositif de contrôle d'attitude d'un engin spatial | |
EP1002716A1 (fr) | Procédé et dispositif de pilotage de l'attitude d'un satellite | |
WO2007042652A1 (fr) | Procede et dispositif pour attenuer sur un aeronef les effets d'une turbulence verticale | |
WO2014122176A1 (fr) | Mini-manche de commande électromagnétique à retour d'effort | |
EP0076179A1 (fr) | Procédé pour aligner l'axe de roulis d'un satellite avec une direction désirée | |
EP1989104B1 (fr) | Systeme de commande electrique pour une gouverne de direction d'un avion | |
CA2383255C (en) | Method of controlling the attitude and stabilization of a satellite in low orbit | |
EP1989113A1 (fr) | Engin spatial et procede pour faire fonctionner l'engin spatial | |
CH355358A (fr) | Appareil de commande de vol pour un engin aérien | |
BE478679A (enrdf_load_html_response) | ||
EP2552782B1 (fr) | Procédé de commande d'un système de contrôle d'attitude et système de contrôle d'attitude d'un véhicule spatial | |
BE479472A (enrdf_load_html_response) | ||
BE479805A (enrdf_load_html_response) | ||
EP0796786A1 (fr) | Procédé et dispositif pour la manoeuvre rapide d'une charge utile embarquée sur une plate-forme spatiale | |
BE478730A (enrdf_load_html_response) | ||
BE478729A (enrdf_load_html_response) | ||
FR3050982A1 (fr) | Module de pilotage de desaturation des roues, dispositif de controle d'attitude d'un engin spatial et procede de desaturation des roues associe | |
EP2522956A1 (fr) | Procédé de gestion automatique d'un gyromètre longitudinal monté sur un engin volant | |
EP1590243A1 (fr) | Dispositif de pilotage de l'attitude d'un satellite par actionneurs gyroscopiques | |
BE479050A (enrdf_load_html_response) | ||
US2315754A (en) | Radio navigator | |
BE481894A (enrdf_load_html_response) | ||
FR3001707A1 (fr) | Mini-manche de commande a retour d'effort |