GB738452A - Navigational training or instruction apparatus - Google Patents

Navigational training or instruction apparatus

Info

Publication number
GB738452A
GB738452A GB2519753A GB2519753A GB738452A GB 738452 A GB738452 A GB 738452A GB 2519753 A GB2519753 A GB 2519753A GB 2519753 A GB2519753 A GB 2519753A GB 738452 A GB738452 A GB 738452A
Authority
GB
United Kingdom
Prior art keywords
latitude
motor
potentiometer
craft
voltage
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
Application number
GB2519753A
Inventor
Albert Ernest Cutler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Communications Patents Ltd
Original Assignee
Communications Patents Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Communications Patents Ltd filed Critical Communications Patents Ltd
Priority to GB2519753A priority Critical patent/GB738452A/en
Publication of GB738452A publication Critical patent/GB738452A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/24Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer including display or recording of simulated flight path
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/20Instruments for performing navigational calculations
    • G01C21/22Plotting boards

Abstract

738,452. Navigational training apparatus. COMMUNICATIONS PATENTS, Ltd. Sept. 11, 1953, No. 25197/53. Class 97 (2). [Also in Groups XXXIII and XXXVIII] In navigational training apparatus for indicating the course of a craft by means of a Mercator chart, voltages corresponding to the east-west and north-south craft co-ordinate ground speeds are fed into the apparatus. The north-south speed component is used to compute the latitude of the craft, the movement of the craft indicator over the chart being controlled as a function of the craft co-ordinate movements and the secant of the latitude. As shown, the craft N-S ground speed voltage is fed over terminal 3 and amplifier 5 to drive a two-phase integrator motor 7 at a speed proportional to the input voltage, proportionality being achieved by a tacho-generator 8 driven by the motor 7 feeding back a rate voltage to the amplifier input. The motor drives through gearing 12 the wipers of potentiometers 13, 14 which are thus positioned continuously according to the craft latitude, being initially set manually by a knob 15. The craft E-W ground speed voltage is fed over terminal 4 to the other ends of potentiometer 13 the centre tap of which, corresponding to zero latitude, is earthed over a resistor 16. The potentiometer is so wound that the output derived from its wiper corresponds to the input E-W ground speed voltage multiplied by the secant of the latitude. This output is applied over an amplifier 22 to an integrator motor 24 which drives through gearing 27 the E-W lead screw 21 for the indicator 17. The motor 24 drives a generator 26 which feeds back a rate voltage to the amplifier 22 to render the motor speed proportional to input voltage. The N-S movement of the indicator 17 relative to the Mercator chart 18 may be effected by a motor similarly controlled in accordance with the N-S ground speed multiplied by secant of latitude but the following arrangement is preferred. Instead of using an integrating motor a follow-up motor 31 is used which drives the N-S lead screw 19 and the wiper of a potentiometer 33 until the voltage derived therefrom balances that derived from potentiometer 14. The potentiometer 14 is connected across an A.C. source 28-29. Its centre tap, representing zero latitude, is earthed, and the potentiometer is contoured so that the output at its wiper, which is set by motor 7 according to the latitude #, is proportional to R. log. tan (0/2 + #/4), the vertical distance on a Mercator chart between latitudes zero and #, where R is the earth's radius. The potentiometer 33 is linear and connected across the same source as potentiometer 14 so that for balance of the system the indicator 17 is set correctly in the N-S direction. Second embodiment, Fig. 2. The N-S and E-W ground speed voltages at terminals 3, 4 respectively are applied via amplifiers 30, 22 directly to the motors 31, 24 driving the N-S and E-W lead screws 19, 21 respectively, the variation of the speed of the recording pen 17 with craft latitude being achieved by varying the voltage applied to the excitation windings 39, 38 of the rate signal generators 32, 26. These excitation windings are fed from an amplifier 40 energized from the wiper of a potentiometer 41 set in accordance with the N-S movement of the indicator 17, i.e. the latitude. The potentiometer is contoured so that its output varies as the cosine of the latitude. As the speeds of the motors 24, 32 vary inversely according to the excitation of their respective generator windings 38, 39 as described in Specification 726,397, [Group XXXVII], these motor speeds in addition to their dependence, respectively, on the E-W and N-S ground speed signals, will also vary as the reciprocal of the cosine, i.e. as the secant of the latitude, as is required for a Mercator chart. The apparatus shown in Fig. 1 may be used with skew Mercator charts.
GB2519753A 1953-09-11 1953-09-11 Navigational training or instruction apparatus Expired GB738452A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2519753A GB738452A (en) 1953-09-11 1953-09-11 Navigational training or instruction apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2519753A GB738452A (en) 1953-09-11 1953-09-11 Navigational training or instruction apparatus

Publications (1)

Publication Number Publication Date
GB738452A true GB738452A (en) 1955-10-12

Family

ID=10223803

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2519753A Expired GB738452A (en) 1953-09-11 1953-09-11 Navigational training or instruction apparatus

Country Status (1)

Country Link
GB (1) GB738452A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1124366B (en) * 1956-06-11 1962-02-22 Link Aviation Inc Aviation training device to imitate the operation of magnetic compasses
FR2464522A1 (en) * 1979-08-27 1981-03-06 Juzhnoe Proizv Obiedin Ship location graphical display - has on-board computer interpreting navigational data to produce position plot on chart

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1124366B (en) * 1956-06-11 1962-02-22 Link Aviation Inc Aviation training device to imitate the operation of magnetic compasses
FR2464522A1 (en) * 1979-08-27 1981-03-06 Juzhnoe Proizv Obiedin Ship location graphical display - has on-board computer interpreting navigational data to produce position plot on chart

Similar Documents

Publication Publication Date Title
US2568719A (en) Control system for aircraft control surface and tab
GB738452A (en) Navigational training or instruction apparatus
US2407325A (en) Range converter
FR2411510A1 (en) DIGITAL-ANALOGUE INTERFACE TO BE INSERTED BETWEEN A TRANSMITTER OF DIGITAL CONTROL SIGNALS AND A MOBILE CONTROL UNIT
FR2430129A1 (en) SYSTEM FOR CONTROLLING THE EXCITATION OF A DIRECT CURRENT MOTOR
GB801842A (en) Improvements in and relating to flight performance computers
US2853800A (en) Navigational training or instruction apparatus
GB1317649A (en) Positioning system
US2818211A (en) Navigational computer and plotter for a mercator projection
GB1342018A (en) Electric motor control systems
US2951374A (en) Position and rate sensitive gyro
US2829446A (en) Apparatus for instruction or training in navigation
US2359866A (en) Variable speed drive apparatus
US2775756A (en) Facsimile recorder computer
US3619579A (en) Time of arrival and ground speed computer
US3139571A (en) Sine-cosine multi-rotation servo
US3602792A (en) Servosystem for analogue plotters
SU538387A1 (en) Device for remote angle transmission
GB880187A (en) Improvements in or relating to methods of titration and titration apparatus
US3145298A (en) Secant function generator
GB755051A (en) Improvements in or relating to electric motor control apparatus suitable for calculating systems
GB1148548A (en) Method and apparatus for determining the direction of motion of a moving object
SU120244A1 (en) Following motor speed synchronization system
US3178682A (en) Aircraft ground position indicator
GB1465595A (en) Fast null balance circuit