GB539224A - Improvements in or relating to the remote control of moving objects by means of radiant energy - Google Patents
Improvements in or relating to the remote control of moving objects by means of radiant energyInfo
- Publication number
- GB539224A GB539224A GB30870/39A GB3087039A GB539224A GB 539224 A GB539224 A GB 539224A GB 30870/39 A GB30870/39 A GB 30870/39A GB 3087039 A GB3087039 A GB 3087039A GB 539224 A GB539224 A GB 539224A
- Authority
- GB
- United Kingdom
- Prior art keywords
- torpedo
- antennae
- axis
- valves
- target
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/222—Homing guidance systems for spin-stabilized missiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/22—Homing guidance systems
- F41G7/2273—Homing guidance systems characterised by the type of waves
- F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/30—Command link guidance systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
- F42B19/01—Steering control
- F42B19/10—Steering control remotely controlled, e.g. by sonic or radio control
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Optical Radar Systems And Details Thereof (AREA)
Abstract
539,224. Aerials. WALTON, G. W. Nov. 27, 1939, No. 30870. [Class 40 (v)] [Also in Groups XXXV, XXIX and XXXVIII] Steering.-A self-propelled object such as a torpedo, aircraft, ship tank or vehicle is controlled by a beam of radiant energy and comprises a mechanism acting in response to deviation of its axis from the direction of received energy whereby fluid valves are differentially actuated to adjust the steering by unbalanced electric currents derived from a system of detectors of the radiation which is carried by the object. The transmitter comprises means for generating and refracting the wavelengths employed in the beam and is adjustable in azimuth and elevation. The object may, for example, be maintained in the beam by one wavelength until near its target when a change in wavelength is used to render it controllable by radiation reflected from the target of the same or a different wavelength. Other wavelengths may be switched on or off to steer the object should it leave the beam or to change the speed. As detector, antennae, photo-cells, bolometers or thermocouples may be used but the preferred arrangement employs wavelengths between 200 microns and one metre with antennae having directional response characteristics provided by reflectors, shields, lenses, apertures, &c. A valve-actuating member 7 is gimbal-mounted about the axis of a torpedo and operates on a series of valves controlling the admission of fluid (including pulverised fuel) to independent power units so that diametrically opposite ones are differentially controlled to provide a steering torque. The member 7 is electromagnetically controlled by windings on a magnetic member 11 which is fixed about the longitudinal axis of the torpedo and may have salient poles or a distributed polyphase winding whereby unbalanced excitation of three or more windings will cause a tilt of the member 7. Fig. 4 shows arrangements of antennae on the tank or nose of a torpedo. Figs. 4c and 4d employ three antennae 34 back tilted with respect to the axis of one torpedo and rendered directional also by reflectors 45 or a cylindrical shield 48 with pins 49 between the antennae and a lens 50 forming a rough image of the source of radiation lying normally on the axis of the torpedo. The torpedo may be spinning on its axis, or not. In either case the arrangement of three detectors 34, 35, 36 with rectifiers shown in Fig. 6 in association with three phase windings 14 on the member 7 and a current source such as a battery or an alternator 55 supplying filament heating circuits and plate current through a rectifier 56 and smoothing condenser 58, will, when the torpedo deviates, furnish a magnetic field, oppositely rotating with the frequency of spinwhich may be zero whereby the member 7 may be tilted to an angle according to the deviation from course and is fixed in space in all conditions. The valves are thereby sequentially operated if the torpedo spins as requisite 'to maintain the direction of target required for correcting course. As shown in Fig. 2, each valve is adjusted by a screwed sleeve turned about the valve spindle by a crank 24 engaging a groove in the member 7 and to permit simultaneous adjustment of all valves each spindle engages its sleeve by a screw of different pitch or hand and carries a gear 21 engaging a common rack (not shown). The arrangement shown in Fig. 6 includes a relay responsive to a beam of a second wavelength employed for reflector control from the target ; the relay charges the antennae connected to the control circuits so that the torpedo is responsible to radiation from ahead. Specification 537,473, [Group XXXIII], is referred to. The Provisional Specification states that naval torpedoes, ships, vehicles, tanks, &c. may have masts carrying the detecting means.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB30870/39A GB539224A (en) | 1939-11-27 | 1939-11-27 | Improvements in or relating to the remote control of moving objects by means of radiant energy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB30870/39A GB539224A (en) | 1939-11-27 | 1939-11-27 | Improvements in or relating to the remote control of moving objects by means of radiant energy |
Publications (1)
Publication Number | Publication Date |
---|---|
GB539224A true GB539224A (en) | 1941-09-02 |
Family
ID=10314414
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30870/39A Expired GB539224A (en) | 1939-11-27 | 1939-11-27 | Improvements in or relating to the remote control of moving objects by means of radiant energy |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB539224A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2959128A (en) * | 1945-06-04 | 1960-11-08 | John R Boykin | Control device |
US2977593A (en) * | 1947-11-04 | 1961-03-28 | Raytheon Co | Dielectric nose cone antenna |
US2996008A (en) * | 1944-09-21 | 1961-08-15 | James A Van Allen | Projectile nose structure |
US3000314A (en) * | 1946-03-19 | 1961-09-19 | Edwin R Sanders | Fuze |
US3027842A (en) * | 1946-03-04 | 1962-04-03 | John J Hopkins | Fuze |
US3064194A (en) * | 1945-04-10 | 1962-11-13 | Jules H Sreb | Radio sonde |
US4207841A (en) * | 1945-05-19 | 1980-06-17 | The United States Of America As Represented By The Secretary Of The Army | Dipole antenna for proximity fuze |
US4685639A (en) * | 1985-12-23 | 1987-08-11 | Ford Aerospace & Communications Corp. | Pneumatically actuated ram air steering system for a guided missile |
-
1939
- 1939-11-27 GB GB30870/39A patent/GB539224A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2996008A (en) * | 1944-09-21 | 1961-08-15 | James A Van Allen | Projectile nose structure |
US3064194A (en) * | 1945-04-10 | 1962-11-13 | Jules H Sreb | Radio sonde |
US4207841A (en) * | 1945-05-19 | 1980-06-17 | The United States Of America As Represented By The Secretary Of The Army | Dipole antenna for proximity fuze |
US2959128A (en) * | 1945-06-04 | 1960-11-08 | John R Boykin | Control device |
US3027842A (en) * | 1946-03-04 | 1962-04-03 | John J Hopkins | Fuze |
US3000314A (en) * | 1946-03-19 | 1961-09-19 | Edwin R Sanders | Fuze |
US2977593A (en) * | 1947-11-04 | 1961-03-28 | Raytheon Co | Dielectric nose cone antenna |
US4685639A (en) * | 1985-12-23 | 1987-08-11 | Ford Aerospace & Communications Corp. | Pneumatically actuated ram air steering system for a guided missile |
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