Air vehicle measurement and control system with upper and down links utilizing different spectrum spreading systems
A measurement and control system and aircraft technology, applied in the field of aircraft measurement and control, can solve the problems of low information transmission rate, limited information volume, short time code, etc., and achieve the effect of increasing frequency hopping rate, reducing synchronization time, and strong anti-interception performance
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- Publication Date
- 2012-10-24
- Estimated Expiration
- Not applicable · inactive patent
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention relates to a measurement and control system using different spreading systems for uplink and downlink, belonging to the field of aircraft measurement and control. Background technique
[0002] Two traditional difficulties in aircraft measurement and control lie in weak signals and high dynamics. Because the volume of the aircraft limits the transmission power of the signal and the long-distance propagation energy attenuation, the signal energy reaching the ground receiver is very weak; and the high dynamics of the aircraft causes the signal reaching the ground receiver to produce Doppler effect. With the continuous development of electronic reconnaissance and countermeasure technology, the aircraft measurement and control system is facing the third difficulty: anti-jamming. At present, the civil aircraft measurement and control system in Europe and the United States and other countries adopts the direct sequence spread spectrum system to...
Examples
Embodiment Construction
[0053] Specific embodiments of the present invention will be described below in conjunction with the accompanying drawings.
[0054] The aircraft measurement and control system using different spread spectrum systems for the uplink and downlink of the present invention is composed of an aircraft part and a ground station part, such as figure 1 Shown:
[0055] The aircraft part is equipped with aircraft parameter data acquisition module 1, data processing module 2, telemetry transmission data frame framing module 3, direct sequence spread spectrum modulation module 4, transmitter 5, transmitting antenna 6, receiving antenna 7, radio frequency front-end module 8, Spread frequency hopping hybrid demodulation module 9 and remote control receiving data frame deframing module 10;
[0056] The ground station part includes an instruction processing module 11, a remote control transmitting data frame framing module 12, a frequency-spreading mixed modulation module 13, a ground station...