Goncharenko et al., 2017 - Google Patents
A method to maneuver aeroballistic missiles under counteractionsGoncharenko et al., 2017
- Document ID
- 15101336788404071613
- Author
- Goncharenko V
- Gorchenko L
- Publication year
- Publication venue
- Journal of Computer and Systems Sciences International
External Links
Snippet
A way to maneuver a high-speed aeroballistic missile (AMB) flying over an area where it can be shot down by enemy air and antimissile weapons is presented. It involves configuring the maneuver and setting reference points' coordinates in a conditional coordinate system in …
- 230000001276 controlling effect 0 abstract description 17
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
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