- •Text 1 naviagtion system – area navigation
- •Naviagtion system – vor/dme
- •Text 2 naviagtion system – satellite
- •Text 3 the effects of the weather on aviation
- •Text 4 the role of radar in atc
- •Text 5 naviagtion system – ins
- •Naviagtion system – ndb
- •Text 6 navigation system – landing aids
- •Text 8 primary radar
- •Text 9 radio navigation aids to final approach and landing ils
- •Text 13 area control service
- •Text 14 the control tower (Part 2)
- •Text 15
- •Text 16
- •Visual aids for navigation marking and lights
- •Text 18 some problems associated with radar (Part 2)
- •Text 19 aeronautical information service (Part 2)
- •Text 21 aims and objectives of icao
- •Text 23 ground and tower control
- •Text 24 holding
- •Text 25 global positioning system (part 1)
Text 1 naviagtion system – area navigation
Computers in the aircraft can integrate
data from many navigational sources and
display a moving type map display of the
aircraft's location. These computers also
allow navigation away from the pre defined
centerlines provided by point source ground
based navigation aids. This concept is known
as Area Navigation (RNAV).
Increasingly flight in specified areas will
require aircraft to be area navigation
equipped. This allows the controllers to use
more flexible routing and to increase the
capacity of the airspace.
Naviagtion system – vor/dme
The VOR (VHF Omnidirectional Radio Range) used in association with the DME (Distance Measuring Equipment) provides a more accurate point source navigation system permitting accurate definition of air routes.
VOR enables a pilot to determine the direction to or from a VOR beacon and, if necessity, approach it on a preselected magnetic heading (QDM). The VOR is also widely used to define holding points and as a non-precision approach aid.
integrate интегрировать, объединять
flexible [7fleksibl]гибкий
omni directional [7Omnidi7rekSEnl]всенаправленный
preselected [7prisE7lektid]предопределённый, назначенный заранее
Text 2 naviagtion system – satellite
Satellite systems are capable of providing very accurate three dimensional position information. In addition to the normal horizontal position information the height of the aircraft can also be determined. Accuracy can be of the order of one or two metres depending on the system and any ancillary equipment used.
Typical of the systems in use today are:
GPS- Global Positioning System (USA), aid
GLONASS - Global Orbiting Navigation Satellite System (CIS)
Together these from the GNSS - Global Navigation Satellite System.
For the moment both systems are managed by the military services of America and Russia. Discussions are under way to provide a civil controlled system. Currently the accuracy available is controlled by the military with their users receiving an accuracy around 12 m whilst civil users are restricted to an accuracy of 100 m.
The addition of a localised ground based satellite receiver that broadcasts correctional information can increase the civil accuracy to around 5 m. This is known as differential GPS.
The development of GNSS based ADS (Automatic Dependent Surveillance) will prove especially useful over sparsely populated and oceanic areas where radar (SSR) coverage is not possible. The position of the aircraft, determined by INS (Inertial Navigation Systems) and satellite systems, is relayed via satellite to a ground station where the signals are processed and can be presented to the controller on a synthetic dynamic display (SDD). Controllers have a virtual ‘radar’ picture of their traffic; Positional accuracy is in the order of 100m.
Satellite navigation will also soon provide sufficient accuracy to enable aircraft to carry out precision approaches and landings, thus reducing the need for ground based systems.
3-dimentional [dai7menSEnl]3-мерный
ancillary [En7silEri]дополнительный, вспомогательный
sparsely [7spa:sli]редко, мало
dynamic [dai7nXmik]динамичный, подвижный
sufficient [sE7fiSEnt]достаточный