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Agile remote sensing satellite multi-target in-orbit observation method

A remote sensing satellite and multi-target technology, applied in the field of agile remote sensing satellite multi-target on-orbit observation

Active Publication Date: 2020-08-11
INNOVATION ACAD FOR MICROSATELLITES OF CAS +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to provide an agile remote sensing satellite multi-target on-orbit observation method to solve how to realize the agile remote sensing satellite on-orbit receiving emergency tasks, to observe multiple point targets and to plan the observation path within a limited time window of one transit

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  • Agile remote sensing satellite multi-target in-orbit observation method
  • Agile remote sensing satellite multi-target in-orbit observation method
  • Agile remote sensing satellite multi-target in-orbit observation method

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Embodiment 1

[0055] This embodiment provides an agile remote sensing satellite multi-target on-orbit observation method, such as figure 1 As shown, the agile remote sensing satellite multi-target on-orbit observation method includes: acquiring multi-target latitude and longitude information, observation weight and observation starting point information as input conditions for mission planning; according to the multi-target latitude and longitude information, observation weight and Observation start point information, combining several consecutive targets in forward observation into a forward observation sequence during forward observation, forming multiple forward chains; according to the longitude and latitude information, observation weight and observation starting point Information, during backward observation, combine several consecutive targets in backward observation into a backward observation sequence, forming multiple backward chains; according to the income of different combinatio...

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Abstract

The invention provides an agile remote sensing satellite multi-target in-orbit observation method, which comprises the steps of acquiring longitude and latitude information, observation weight and observation starting point information of multiple targets as input conditions of task planning; during forward observation, combining several continuous targets in forward observation into a forward observation sequence so as to form a plurality of forward chains; during backward observation, combining several continuous targets in backward observation into a backward observation sequence so as to form a plurality of backward chains; according to the earnings after different forward chains and backward chains are combined, determining a combination of the forward chains and the backward chains by combining the attitude maneuver cost generated in the observation direction, adjusting the number of targets on the forward chains or the backward chains according to the combination of the forwardchains and the backward chains, calculating a switching point of the combination, forming a complete observation sequence in the transit period, and completing task planning.

Description

technical field [0001] The invention relates to the technical field of agile remote sensing satellites, in particular to a multi-target on-orbit observation method for agile remote sensing satellites. Background technique [0002] With the development of agile satellites, the attitude maneuvering ability of agile satellites is getting stronger and stronger. For emergencies, it can quickly point to a specific area through rapid attitude maneuvering, and continuously observe the mission area through regional gaze. However, the response to the mission requires real-time on-orbit planning capabilities, and timely and reasonable scheduling of satellite resources to achieve the highest possible observation benefits. A large number of point targets to be observed in a wide range are formed by wide-width payloads or other information, and the flying agile satellites obtain the position information and status evaluation information of these point targets from the ground or the inter-...

Claims

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Application Information

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IPC IPC(8): G01C21/20G01C21/24
CPCG05D1/0833
Inventor 张晟宇孙煜坤胡海鹰朱振才封家鹏
Owner INNOVATION ACAD FOR MICROSATELLITES OF CAS
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