Most
modern navigation relies primarily on positions determined electronically by receivers collecting information from satellites. Most other modern techniques rely on finding intersecting
lines of position or LOP. A line of position can refer to two different things, either a line on a chart or a line between the observer and an object in real life. A bearing is a measure of the direction to an object. Lines (or circles) of position can be derived from a variety of sources: • celestial observation (a short segment of the
circle of equal altitude, but generally represented as a line), • terrestrial range (natural or man made) when two charted points are observed to be in line with each other, • compass bearing to a charted object, • radar range to a charted object, • on certain coastlines, a depth sounding from
echo sounder or hand
lead line. There are some methods seldom used today such as the maritime method of "dipping a light" to calculate the geographic range from observer to lighthouse, where the height of the lighthouse is known (from a list of lights or from a chart). Methods of navigation have changed through history. Each new method has enhanced the mariner's ability to complete his voyage.
Piloting Piloting (also called pilotage) involves navigating an aircraft by visual reference to landmarks, or a water vessel in restricted waters and fixing its position as precisely as possible at frequent intervals. More so than in other phases of navigation, proper preparation and attention to detail are important. It may also involve navigating a ship within a river,
canal or
channel in close proximity to land. By knowing which point on the rotating Earth a celestial object is above and measuring its height above the observer's horizon, the navigator can determine his distance from that subpoint using mathematical calculation. A
nautical almanac and a source of time, typically a
marine chronometer are used to compute the subpoint on Earth a celestial body is over, and a
sextant is used to measure the body's angular height above the horizon. A navigator shoots a number of stars in succession to give a series of overlapping lines of position. Where they intersect is the celestial fix. The Moon and Sun may also be used. The Sun can also be used by itself to shoot a succession of lines of position (best done around local noon) to determine a position.
Marine chronometer In order to accurately measure longitude, the precise time is required of a sextant sighting (down to the second, if possible) which is then recorded for subsequent calculation. Each second of error is equivalent to 15 seconds of longitude error, which at the equator is a position error of .25 of a nautical mile, about the accuracy limit of manual celestial navigation. The spring-driven marine chronometer is a precision timepiece used aboard ship to provide accurate time for celestial observations. A chronometer differs from a spring-driven watch principally in that it contains a variable lever device to maintain even pressure on the mainspring, and a special balance designed to compensate for temperature variations. The second mirror, referred to as the "horizon glass", is fixed to the front of the frame. One half of the horizon glass is silvered and the other half is clear. Light from the celestial body strikes the index mirror and is reflected to the silvered portion of the horizon glass, then back to the observer's eye through the telescope. The observer manipulates the index arm so the reflected image of the body in the horizon glass is just resting on the visual horizon, seen through the clear side of the horizon glass.
Bubble octant Until the widespread usage of technologies such as inertial navigation systems,
VHF omnidirectional range and GNSS, air navigators used the
Bubble octant or bubble sextant. Using this instrument to take sights, mathematical calculations could then be carried out to determine the past position of the aircraft.
Inertial navigation Inertial navigation system (INS) is a
dead reckoning type of navigation system that computes its position based on motion sensors. Before actually navigating, the initial latitude and longitude and the INS's physical orientation relative to the Earth (e.g., north and level) are established. After alignment, an INS receives impulses from motion detectors that measure (a) the acceleration along three axes (accelerometers), and (b) rate of rotation about three orthogonal axes (gyroscopes). These enable an INS to continually and accurately calculate its current latitude and longitude (and often velocity). Advantages over other navigation systems are that, once aligned, an INS does not require outside information. An INS is not affected by adverse weather conditions and it cannot be detected or jammed. Its disadvantage is that since the current position is calculated solely from previous positions and motion sensors, its errors are cumulative, increasing at a rate roughly proportional to the time since the initial position was input. Inertial navigation systems must therefore be frequently corrected with a location 'fix' from some other type of navigation system. The first inertial system is considered to be the V-2 guidance system deployed by the Germans in 1942. However, inertial sensors are traced to the early 19th century. The advantages INSs led their use in aircraft, missiles, surface ships and submarines. For example, the U.S. Navy developed the Ships Inertial Navigation System (SINS) during the
Polaris missile program to ensure a reliable and accurate navigation system to initial its missile guidance systems. Inertial navigation systems were in wide use until
satellite navigation systems (GPS) became available. INSs are still in common use on submarines (since GPS reception or other fix sources are not possible while submerged) and long-range missiles but are not now widely found elsewhere.
Gravity-aided navigation Gravity-aided navigation originated in the 1990s and provides a technology to obtain a position fix for navigation. It utilises the concept that an onboard sensor measures elements of the gravitational vector while the platform is in motion and then these measurements are referenced to a map of the
Earth's gravitational field to determine a position.
Space navigation Not to be confused with satellite navigation, which depends upon satellites to function, space navigation refers to the navigation of spacecraft themselves. This has historically been achieved (during the
Apollo program) via a
navigational computer, an Inertial navigation system, and via celestial inputs entered by astronauts which were recorded by sextant and telescope. Space rated navigational computers, like those found on Apollo and later missions, are designed to be hardened against possible data corruption from radiation. Navigation in space has three main components: the use of a suitable reference trajectory which describes the planned flight path of the spacecraft, monitoring the actual spacecraft position while the mission is in flight (orbit determination) and creating maneuvers to bring the spacecraft back to the reference trajectory as required (flight path control). Another possibility that has been explored for deep space navigation is
Pulsar navigation, which compares the X-ray bursts from a collection of known pulsars in order to determine the position of a spacecraft. This method has been tested by multiple space agencies, such as
NASA and
ESA.
Electronic navigation Radar navigation Radars can be used for navigation and
marine radars are commonly fitted to ships for navigation at sea. Radar is an effective aid to navigation because it provides ranges and bearings to objects within range of the radar scanner. When a vessel (ship or boat) is within radar range of land or fixed objects (such as special radar aids to navigation and navigation marks) the navigator can take distances and angular bearings to charted objects and use these to establish arcs of position and lines of position on a chart. A fix consisting of only radar information is called a radar fix. Types of radar fixes include "range and bearing to a single object," "two or more bearings," This technique involves creating a line on the screen that is parallel to the ship's course, but offset to the left or right by some distance. Other techniques that are less used in general navigation have been developed for special situations. One, known as the "contour method," involves marking a transparent plastic template on the radar screen and moving it to the chart to fix a position. Another special technique, known as the Franklin Continuous Radar Plot Technique, involves drawing the path a radar object should follow on the radar display if the ship stays on its planned course. During the transit, the navigator can check that the ship is on track by checking that the pip lies on the drawn line. Due to the success of the
Global Positioning System the use of Omega declined during the 1990s, to a point where the cost of operating Omega could no longer be justified. Omega was terminated on September 30, 1997, and all stations ceased operation. LORAN is a terrestrial
navigation system using
low frequency radio transmitters that use the time interval between radio signals received from three or more stations to determine the position of a ship or aircraft. The current version of LORAN in common use is LORAN-C, which operates in the
low frequency portion of the EM spectrum from 90 to 110
kHz. Many nations are users of the system, including the
United States,
Japan, and several European countries. Russia uses a nearly exact system in the same frequency range, called
CHAYKA. LORAN use is in steep decline, with
GPS being the primary replacement. However, there are attempts to enhance and re-popularize LORAN. LORAN signals are less susceptible to interference and can penetrate better into foliage and buildings than GPS signals.
Satellite navigation A GNSS allow small
electronic receivers to determine their location (
longitude,
latitude, and
altitude) within a few meters using
time signals transmitted along a
line of sight by
radio from
satellites. The first system, GPS was developed by the
United States Department of Defense and officially named NAVSTAR GPS (NAVigation Satellite Timing And Ranging Global Positioning System). The
satellite constellation is managed by the
United States Air Force 50th Space Wing. The cost of maintaining the system is approximately
US$750 million per year, including the replacement of aging satellites, and research and development. Despite this fact, GPS is free for civilian use as a
public good. With improvements in technology and developments globally, as of 2024, there are several different operational GNSS now available for navigation by the public. These include the
United States NAVSTAR
Global Positioning System (GPS), the
Russian
GLONASS, the
European Union's
Galileo positioning system and the
Beidou navigation system of
China. Typically a
compass is also provided to determine direction when not moving.
Acoustic navigation Acoustic location is a method of navigation by the use of acoustic positioning systems which determine the position of an object by using
sound waves. It is primarily used by
submarines and ships fitted with
sonar and similar transducer based technologies.
Underwater acoustic positioning systems are also commonly used by divers and
Remotely operated underwater vehicles, specifically the
Long baseline acoustic positioning system, the
Short baseline acoustic positioning system and the
Ultra-short baseline acoustic positioning system. ==Navigation processes==