JPS6489722A - Artificial sattelite future state supposing device - Google Patents

Artificial sattelite future state supposing device

Info

Publication number
JPS6489722A
JPS6489722A JP62246093A JP24609387A JPS6489722A JP S6489722 A JPS6489722 A JP S6489722A JP 62246093 A JP62246093 A JP 62246093A JP 24609387 A JP24609387 A JP 24609387A JP S6489722 A JPS6489722 A JP S6489722A
Authority
JP
Japan
Prior art keywords
sattelite
artificial
condition
output
supposing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP62246093A
Other languages
Japanese (ja)
Inventor
Masaru Oka
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toshiba Corp
Original Assignee
Toshiba Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toshiba Corp filed Critical Toshiba Corp
Priority to JP62246093A priority Critical patent/JPS6489722A/en
Publication of JPS6489722A publication Critical patent/JPS6489722A/en
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Selective Calling Equipment (AREA)
  • Radio Relay Systems (AREA)

Abstract

PURPOSE:To automatically suppose the future condition of an artificial sattelite mounting device by fetching the telemetry value from an artificial sattelite for a constant time and supposing the change rate of the telemetry value and the telemetry value in the present and future. CONSTITUTION:For the telemetry value from the output of a condition supposing adding register 7 from an artificial sattelite, the difference is detected for a T second in an adder 6. The difference is weighted and added to a change rate adding register 8 for a T second. The output of the change rate adding register 8 is added to the condition supposing adding register 7 for one second. Consequently, in a stationary balancing condition, the output of the condition supposing adding register 7 becomes equal approximately to the telemetry value. The output of the change rate adding register 8 is made n-fold in a multiplier 10, this and the output of the condition supposing adding register 7 are added by an adder 11, and then, as the result, the telemetry value after (n) seconds is supposed.
JP62246093A 1987-09-30 1987-09-30 Artificial sattelite future state supposing device Pending JPS6489722A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62246093A JPS6489722A (en) 1987-09-30 1987-09-30 Artificial sattelite future state supposing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62246093A JPS6489722A (en) 1987-09-30 1987-09-30 Artificial sattelite future state supposing device

Publications (1)

Publication Number Publication Date
JPS6489722A true JPS6489722A (en) 1989-04-04

Family

ID=17143384

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62246093A Pending JPS6489722A (en) 1987-09-30 1987-09-30 Artificial sattelite future state supposing device

Country Status (1)

Country Link
JP (1) JPS6489722A (en)

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