Apparatus for estimating slant visibility in fog

• US 4,419,731 A
• Filed: 11/17/1980
• Issued: 12/06/1983
• Est. Priority Date: 03/19/1979
• Status: Expired due to Term

• Current Assignee: The secretary of state for defence in her Britannic Majesty's Government of the United Kingdom of Great Britain And Northern Ireland
• Original Assignee: The secretary of state for defence in her Britannic Majesty's Government of the United Kingdom of Great Britain And Northern Ireland
• Inventors: Puffett, Alan W.
• Primary Examiner(s): Krass, Errol A.
• Application Number:
  US06/224,563
• Time in Patent Office: 1,114 Days
• Field of Search: 364/428-430, 364/433, 364/435, 364/578, 73/170 R, 343/5 W, 356/4
• US Class Current: 701/16
• CPC Class Codes: G01N 21/538 for determining atmospheric attenuation and visibility
• CPC Class Codes: G01W 1/00 Meteorology

Abstract

Apparatus for estimating the slant visibility in obscured atmospheres such as fog, whereby an indication is derived as to when, during an aircraft landing approach in such conditions, the aircrew are likely to be able to see the runway lights. The apparatus comprises a transmissometer array arranged to take visibility readings over a slanted distance from different heights not far from a runway threshold, and a computer arranged to compare the readings with a plurality of fog profile models, to determine the definitive model and hence to derive and indicate a visual acquisition estimate.

Claims

1. An apparatus for estimating slant visual range in fog comprising:

a transmissometer array, having at least three transmissometer elements at respectively greater differing heights h₁, h₂ and h₃ above the ground and disposed for operation between the differing heights and ground level, for generating transmissometer signals indicative of a fog strength; and

a slant visual range (SVR) computer coupled to said transmissometer array so as to receive the transmissometer signals therefrom, said SVR computer having;

means for converting the transmissometer signals into signals σ

h₁, σ

h₂, σ

h₃ representing the mean integral of extinction coefficient between said respectively greater heights h₁, h₂, h₃, above ground and ground level;

means for storing a predetermined set of extinction coefficient σ

_h function models, each model characterising a different type of fog pattern, each model having predetermined criteria for its selection and use, and containing at least one empirical constant;

means for selecting one of the models in accordance with values of σ

h₁, σ

h₂, σ

h₃ determined by said converting means;

means for determining the values of the empirical constant in the selected model thus obtaining a definitive extinction coefficient profile,

means for storing values representing airfield lighting and accepting values representing flight path and background brightness, and

means for estimating slant visual range from the definitive profile and the airfield lighting, background brightness and flight path values.

2. An apparatus according to claim 1 and wherein said converting means comprises means for converting the transmissometer array signals into σ

_h signals in accordance with the function;

##EQU10## where R is the distance over which the measurement is taken;

I_h is the signal from said transmissometer array, and

I_o is a clear day datum transmissometer signal.

3. An apparatus according to claim 1 wherein the means for storing function models comprises means for storing the following predetermined set of models and their respective predetermined criteria for selection and use:

##EQU11## where a, b, c, j, k, p, q, r are empirical constants and σ

_h.sbsb.U and σ

_h.sbsb.L are mean integrals of extinction coefficient between the ground and a height above and below the fog top respectively.

4. An apparatus according to claim 1 further including means for determining a visual sequence from the selected σ

_h function model.

5. An apparatus according to claim 1 wherein said deriving means includes means for determining the intersection of the function:

##EQU12## with the definitive model, where γ and

α

are empirical constant respectively related to a flight path about and lighting pattern characteristics of an airport;

E_T represents an eye illuminance threshold, measured in lux, and

σ

h_c is the mean integral of the extinction coefficient profile at the visual contact height.

6. An apparatus according to claim 5 further comprising means for deriving the value Log₁₀ (E_T) for use in the H_c function when the value of E_T is not known, from the function:

space="preserve" listing-type="equation">Log.sub.10 (E.sub.T)=u log.sub.10 β

-v,

where

β

represents background brightness in nits and u and v are empirical constants.

7. An apparatus according to claim 1 further comprising a brightness measuring detector mounted on the transmissometer array for deriving the value of β

.

8. An apparatus according to claim 6 and further comprising means for comparing the value of Log₁₀ (E_T) with a value -w and for limiting the value of Log₁₀ (E_T)≧

-w, where w is an accustomation factor for night use, the limited value being used in the H_c function.

9. Apparatus according to claim 5 further comprising:

means for storing aircraft configuration data;

means for applying the aircraft configuration data to the derived H_c value; and

means for modifying the H_c function in accordance with the aircraft configuration data.

10. Apparatus according to claim 4 wherein the SVR computer comprises iteratively operable means for applying to the selected model, the particular lighting patterns, direction, intensity and visual threshold values at a sequence of aircraft positions, during a landing run.

11. An apparatus according to claim 1 wherein said transmissometer elements disposed for operation at three different heights above the ground comprise reflector elements.

12. An apparatus according to claim 1 wherein said transmissometer array comprises a source/detector transmissometer unit mounted substantially at ground level and a plurality of reflector elements mounted at different heights.

13. An apparatus according to claim 1 wherein h₃ is substantially 30 meters.

14. An apparatus according to claim 1 wherein said transmissometer array is mounted on a tower disposed at least 370 meters laterally from the center line of a runway.

15. An apparatus according to claim 1 wherein said transmissometer array is mounted on a tower disposed at least 350 meters ahead of a runway threshold.

16. An apparatus according to claim 1 further including a distinct transmissometer separate from said transmissometer array and for substantially horizontal operation up to 4 meters above ground to provide a confirmation of the fog extent and of the σ

_h profile estimate.

17. An apparatus for estimating slant visual range in fog, comprising:

a transmissometer array disposed for slant operation and having reflector elements disposed at respectively greater different heights h₁, h₂ and h₃ above ground and a source/detector unit transmissometer unit mounted substantially at ground level, said array being arranged for generating signals indicative of a fog structure;

a background brightness detector, and

signal processing means, arranged for receiving said signals derived from said transmissometer array and signals representing background brightness from said brightness detector and for estimating slant visual range, said signal processing means comprising;

converter means for converting the transmissometer signals into signals σ

h₁, σ

h₂, σ

h₃ representing the mean integral of extinction coefficient between the respectively greater heights h₁, h₂, h₃, (and the ground, said converter means for converting) in accordance with the function ##EQU13## where R is the distance over which the measurement is taken,

I_h is the fog structure indicative signal from the transmissometer in respect of a height h₁, h₂, h₃, and

I_o is a clear day datum transmissometer signal, comparison means for comparing the σ

h signals and selecting one model from the following groups of three (3) models in accordance with the predetermined criteria associated with each model ##EQU14## where a, b, c, j, k, p, q, r are empirical constants and σ

h_U and σ

h_L are mean integrals of extinction coefficient between the ground and a height above and below the fog top respectively,

determining means, coupled to said comparison means, for determining the values of the empirical constants in the selected model to establish a definitive model,

store means for storing values representing airfield lighting and accepting values representing flight path,

Log₁₀ (E_T) deriving means operative to determine the value of Log₁₀ (E_T) from the function

space="preserve" listing-type="equation">Log.sub.10 (E.sub.T)=u log.sub.10 β

-v

where E_T represents the eye illuminance threshold, measured in lux, β

represents background brightness in nits and u and v are empirical constants;

(and)

Visual contact height determining means coupled to said Log₁₀ (E_T) determining means, for determining the intersection of the function ##EQU15## with the definitive model, where γ and

α

are empirical constants respectively related to flight path about the lighting pattern of an airport, and iterative visual sequence determination means coupled to said comparison means and to said store means for providing a visual sequence.