SU551919A1 - Method of determining aircraft inertia moment - Google Patents

Method of determining aircraft inertia moment

Info

Publication number
SU551919A1
SU551919A1 SU7301896116A SU1896116A SU551919A1 SU 551919 A1 SU551919 A1 SU 551919A1 SU 7301896116 A SU7301896116 A SU 7301896116A SU 1896116 A SU1896116 A SU 1896116A SU 551919 A1 SU551919 A1 SU 551919A1
Authority
SU
USSR - Soviet Union
Prior art keywords
inertia moment
determining aircraft
aircraft inertia
determining
moment
Prior art date
Application number
SU7301896116A
Other languages
Russian (ru)
Inventor
В.А. Савичев
Original Assignee
Savichev V A
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 Savichev V A filed Critical Savichev V A
Priority to SU7301896116A priority Critical patent/SU551919A1/en
Application granted granted Critical
Publication of SU551919A1 publication Critical patent/SU551919A1/en

Links

SU7301896116A 1973-03-23 1973-03-23 Method of determining aircraft inertia moment SU551919A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU7301896116A SU551919A1 (en) 1973-03-23 1973-03-23 Method of determining aircraft inertia moment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU7301896116A SU551919A1 (en) 1973-03-23 1973-03-23 Method of determining aircraft inertia moment

Publications (1)

Publication Number Publication Date
SU551919A1 true SU551919A1 (en) 1978-06-25

Family

ID=20546205

Family Applications (1)

Application Number Title Priority Date Filing Date
SU7301896116A SU551919A1 (en) 1973-03-23 1973-03-23 Method of determining aircraft inertia moment

Country Status (1)

Country Link
SU (1) SU551919A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110723309A (en) * 2019-08-27 2020-01-24 广东工业大学 Method for measuring rotational inertia of quad-rotor unmanned aerial vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110723309A (en) * 2019-08-27 2020-01-24 广东工业大学 Method for measuring rotational inertia of quad-rotor unmanned aerial vehicle

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