IP Library Granted Patent US 12,291,356
Granted Patent B2
US 12,291,356 · App. 17/785,242 · Granted May 6, 2025

Safe landing point search device for searching for safe landing point by using contour line information with respect to terrain map, and safe landing point search method

Inventors: Youeyun Jung (Daejeon, KR); Hyochoong Bang (Daejeon, KR); Seongheon Lee (Daejeon, KR)
Assignee: KOREA AEROSPACE RESEARCH INSTITUTE
B64G1/62B64G1/66
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,291,356
App. No.
17/785,242
Granted
May 6, 2025
Kind
B2
Abstract

A safe landing point search device for searching for a safe landing point of an unmanned exploration device that lands on and explores a celestial body, includes a terrain map obtaining unit configured to obtain a terrain map, a contour line generating unit configured to generate contour lines based on a reference minimum height value and a height interval value by using the terrain map, a largest empty circle (LEC) searching unit configured to search for one or more LECs having a radius greater than or equal to a lower-limit radius in a contour line map including the contour lines, and a safe landing point outputting unit configured to output a safe landing point having a largest radius among the one or more LECs and transmit the safe landing point to the unmanned exploration device.

Claims (28)

1. A landing method of an unmanned exploration device comprising:

executing, by a safe landing point search device having a processor, operations for searching a safe landing point in a scanning area of an unmanned exploration device, wherein the operations comprise:

obtaining, by the safe landing point search device, a terrain map of a planned landing point;

generating, by the safe landing point search device, a plurality of contour lines in the obtained terrain map,

wherein each of the plurality of contour lines connects points having a same height in the obtained terrain map and represents a height different from other contour lines, and

wherein the plurality of contour lines comprises a first number (L) of contour line groups based on predetermined criteria, wherein the predetermined criteria include a reference minimum height value, a reference maximum height value, a preset minimum interval value, and a preset height interval value, by using the obtained terrain map, wherein the first number (L) of contour line groups is determined by dividing the preset height interval value by the preset minimum value, and the preset height interval value is set equal to a threshold height enabling safe landing; and

wherein each of the first number (L) of contour line groups includes a second number (M) of contour lines, separated by the preset height interval value, between the reference minimum height value and the reference maximum height value, and each height of the second number (M) of contour lines in each of the first number (L) of contour line groups does not overlap;

generating, by the safe landing point search device, the first number (L) of contour line maps, wherein each contour line map includes the second number (M) of contour lines belonging to each of the first number (L) of contour line groups and represents terrain conditions at different heights corresponding to a respective contour line of the second number (M) of contour lines; and

detecting, by the safe landing point search device, a largest empty circle (LEC) having a radius greater than or equal to a lower-limit radius in each of the first number (L) contour line maps, wherein the lower-limit radius is determined using the threshold height enabling safe landing; and

determining, by the safe landing point search device, a real-time hazard by using surrounding terrain information obtained from at least the terrain map, a sensor unit and a laser;

determining, by the safe landing point search device, the safe landing point in the planned landing point based on a largest radius among the first number (L) of LECs and a plurality of parameters including a diameter of the unmanned exploration device, field of view, measuring altitude, and margin related to the scanning area, and the real-time hazard;

outputting, by the safe landing point search device, the safe landing point having no real-time hazard and transmitting the safe landing point to the unmanned exploration device; and

enabling, by the safe landing point search device, landing of the unmanned exploration device on the safe landing point that is geographically safe and includes no valley or steep slope.

2. The landing method of claim 1 , wherein the lower-limit radius is calculated by using a slope threshold value with respect to the threshold height that enables safe landing.

3. A non-transitory computer-readable recording medium storing therein an operating program that causes a safe landing point search device having a processor to execute a process comprising:

executing operations for searching a safe landing point in a scanning area of an unmanned exploration device, wherein the operations comprise:

obtaining a terrain map of a planned landing point;

generating a plurality of contour lines in the obtained terrain map,

wherein each of the plurality of contour lines connects points having a same height in the obtained terrain map and represents a height different from other contour lines, and

wherein the plurality of contour lines comprises a first number (L) of contour line groups based on predetermined criteria, wherein the predetermined criteria include a reference minimum height value, a reference maximum height value, a preset minimum interval value, and a preset height interval value by using the terrain map, wherein the first number (L) of contour line groups is determined by dividing the preset height interval value by the preset minimum interval value, and

wherein the first number (L) of contour line groups include a second number (M) of contour lines, separated by the preset height interval value, between the reference minimum height value and the reference maximum height value, and each height of the second number (M) of contour lines does not overlap and the preset height interval value is set equal to a threshold height enabling safe landing;

generating the first number (L) of contour line maps, wherein each contour line map includes the second number (M) of contour lines belonging to each of the first number (L) of contour line groups and represents terrain conditions at a different height corresponding to a respective contour line of the second number (M) of contour lines; and

detecting a largest empty circle (LEC) having a radius greater than or equal to a lower-limit radius in each of the first number (L) of contour line maps, wherein the lower-limit radius is determined using the threshold height enabling safe landing;

determining a real-time hazard by using surrounding terrain information obtained from at least the terrain map, a sensor unit and a laser;

determining the safe landing point in the planned landing point based on a largest radius among the first number (L) of LECs and a plurality of parameters including a diameter of the unmanned exploration device, field of view, measuring altitude, and margin related to the scanning area, and the real-time hazard;

outputting the safe landing point having no real-time hazard and transmitting the safe landing point to an unmanned exploration device; and

enabling landing of the unmanned exploration device on the safe landing point that is geographically safe and includes no valley or steep slope.

4. The non-transitory computer-readable recording medium of claim 3 , wherein the lower-limit radius is calculated by using a slope threshold value with respect to the threshold height that enables safe landing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 14, 2022
From: JUNG, YOUEYUN; BANG, HYOCHOONG; LEE, SEONGHEON
To: KOREA AEROSPACE RESEARCH INSTITUTE
Reel/Frame 060197/0161 →
Priority Claims (1)
KR 10-2019-0143976 · Nov 12, 2019 · national
Continuity (1)
Related Publication 20230348115A1 · Nov 2, 2023
References Cited (15)
US 6167144A · Nishiguchi et al. · 2000 [cited by applicant]
US 6216065B1 · Hall · 2001 [cited by examiner]
US 10029804B1 · Chamberlain · 2018 [cited by examiner]
US 20080023587A1 · Head et al. · 2008 [cited by applicant]
US 20170162061A1 · Srivastav · 2017 [cited by examiner]
US 20190002122A1 · Ding · 2019 [cited by examiner]
US 20190248487A1 · Holtz · 2019 [cited by examiner]
US 20220024582A1 · Nakazawa · 2022 [cited by examiner]
JP 05039095A · 1993 [cited by applicant]
JP 11105797A · 1999 [cited by applicant]
KR 1020130133480A · 2013 [cited by applicant]
KR 1020160112080A · 2016 [cited by applicant]
International Search Report and Written Opinion issued in corresponding International Application No. PCT/KR2020/003782, mailed Jul. 29, 2020, 16 pages. [cited by applicant]
Jung et al., Digital Terrain Map Based Safe Landing Site Selection for Planetary Landing, IEEE Transactions on Aerospace and Electronic System, Apr. 2019, pp. 368-380, vol. 56 (1). [cited by applicant]
Grant of Patent issued in corresponding Korean Application No. 10-2019-0143976, issued Nov. 26, 2020, 6 pages, and an English translation thereof, 2 pages. [cited by applicant]