Altitude detecting unit, loading/driving apparatus, and altitude detecting method

• US 9,594,169 B2
• Filed: 08/20/2015
• Issued: 03/14/2017
• Est. Priority Date: 08/20/2014
• Status: Active Grant

• Current Assignee: Horiba Limited
• Original Assignee: Horiba Limited
• Inventors: Fukami, Shun, Uratani, Katsumi
• Primary Examiner(s): Jeanglaud, Gertrude Arthur
• Application Number:
  US14/831,507
• Publication Number:
  US 20160054451A1
• Time in Patent Office: 572 Days
• Field of Search: 701/4, 701/9, 701/14, 701/15, 701/469, 340/970, 340/977, 342/357.28
• US Class Current: 1/1
• CPC Class Codes: G01C 5/06 by using barometric means
• CPC Class Codes: G01M 17/007 Wheeled or endless-tracked vehicles G01M17/08 takes precedence
• CPC Class Codes: G01S 19/45 by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement

Abstract

The present invention intends to provide an altitude detecting unit capable of, while utilizing both the advantages of a satellite positioning system and a pressure sensor, making an altitude measurement error, which may occur when combining them, as small as possible, and provide the others, and has determined a conversion expression adapted to convert from pressure into altitude such that at each of multiple valid altitude measurement points at which a satellite positioning system detects accurate altitude, altitude based on pressure is made equal to altitude by the satellite positioning system.

Claims

1. An altitude detecting unit that detects altitude of a running vehicle along a test running route, the altitude detecting unit comprising:

a reception circuit that receives data indicating altitude of the vehicle from a satellite positioning system receiver, and data indicating pressure around the vehicle from a pressure sensor, the satellite positioning system receiver and the pressure sensor both being mounted on the test vehicle during running of a test;

a conversion expression generating circuit that generates a conversion expression for converting data indicating pressure around the vehicle from the pressure sensor, into data indicating the altitude of the vehicle; and

an altitude calculation circuit that converts the data indicating pressure around the vehicle based on the conversion expression into data indicating altitude, and thereby calculates the altitude of the vehicle at a part of or along the whole of the test running route of the vehicle,

the altitude detecting unit being configured such that at each one of multiple predetermined valid altitude measurement points at which valid altitude data is outputted from the receiver along the test running route, pressure altitude, that is altitude obtained by converting pressure data using the conversion expression, is made substantially equal to altitude indicated by valid altitude data.

2. The altitude detecting unit according to claim 1, wherein:

in a satellite positioning invalid section, being a section where valid altitude data is not outputted from the receiver, the conversion expression generating circuit regards a point just before and a point just after a satellite positioning invalid section as two valid altitude measurement points, and the conversion expression generating circuit generates a conversion expression corresponding to the satellite positioning invalid section based on the valid altitude measurement points; and

the altitude calculation circuit selects and fixes the pressure altitude values, obtained by converting pressure indicated by pressure data in the section on a basis of the conversion expression, for invalid sections of the test running route, and selects and fixes the altitude indicated by altitude data, obtained by the receiver, for valid sections of the test running route, valid sections being sections where valid altitude data outputted from the receiver is available.

3. The altitude detecting unit according to claim 1, wherein:

the altitude calculation circuit uses the pressure altitude to also calculate gradients of a part of the test running route or along the whole of the test running route.

4. A loading/driving apparatus for testing a vehicle or a part of the vehicle,

the loading/driving apparatus calculating loads or driving forces acting on the vehicle or the part of the vehicle during a test run on a basis of the gradients of the test running route, the gradients being detected by the altitude detecting unit according to claim 3, and making the calculated loads or driving forces act on the vehicle or the part of the vehicle during the test.

5. An altitude detecting method that detects altitude of a running vehicle along a test route, the altitude detecting method comprising:

receiving data indicating altitude of the vehicle from a satellite positioning system receiver, and data indicating pressure around the vehicle from a pressure sensor, the satellite positioning system receiver and the pressure sensor both being mounted on the test vehicle during running of a test;

generating a conversion expression for converting data indicating pressure around the vehicle, from the pressure sensor, into data indicating the altitude of the vehicle, and making pressure altitude, that is altitude obtained by converting pressure data using the conversion expression, substantially equal to altitude indicated by valid altitude data, at each one of multiple predetermined valid altitude measurement points at which valid altitude data is obtained along the test running route,

converting the data indicating pressure around the vehicle based on the conversion expression into data indicating altitude, and thereby calculating the altitude of the vehicle at a part of or along the whole of the test running route of the vehicle.