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^4fA Contribution to the Levelling of Inertial Navigation Platforms

机译:^ 4FA对惯性导航平台的平整的贡献

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^7fDue to the relatively high speed and low costs at which measurements can be made an airborne gravity system provides an attractive alternative to conventional terrestrial and space based methods to determine the gravity field of the earth. An aircraft provides access to difficult terrain and uniform sampling, but the success of land and sea gravimetry cannot be transferred to airborne gravimetry easily. In the beginning of airborne surveys a number of difficulties emerged and aircraft applications seemed not to be very auspicious. The circumstances were and are a big challenge on flight measurement technology and filtering techniques. This has driven the research program in airborne gravimetry at the Institute of Flight Guidance and Control (IFF) since 1986. The focus of the airborne gravimetry programme at the IFF has been on the development, improvement and application of long-range surveying techniques. It is of particular importance for the future of airborne gravimetry to increase accuracy and resolution. Additionally the IFF is involved in the development of a gravity measurement system using an inertial platform, a gravity sensor, a barometric sensor and kinematic differential carrier phase based GPS positioning. Airborne gravimetry is an important part of inertial flight measurement technique. The principle of using an inertial navigation system to measure the gravity field can be found in [1], [2], [3]. The gravity disturbance signal may be obtained from the time-synchronised difference between the measurements of a precise inertial accelerometer signal (gravity sensor) and an altimeter signal (GPS differential carrier phase, barometric sensor). The gravity sensor measures specific force, which is composed of a gravity component and an aircraft acceleration component. The Global Positioning system (GPS) measures the aircraft motion only. Accuracy requirements for users in geodesy and solid earth geophysics, oceanography and exploration geophysics are described in [4]. An accuracy of 0.5 mGat to 1 mGal in the wavelength range between 1 km and 10 km is for special interest to oil exploration, white an accuracy of 1 mGal to 3 mGal in the wavelength between 10 km and 100 km is important to geodesy.
机译:^ 7Fdue以相对高的速度和低成本,测量的空气传播重力系统提供了传统的地面和空间的方法,以确定地球的重力场。飞机提供困难地形和统一采样的进入,但陆地和海洋重量的成功不能轻易转移到空气传播的重量。在空中的开始,调查出现了许多困难,飞机应用似乎并不是非常吉祥。这种情况是对飞行测量技术和过滤技术来说是一个很大的挑战。这使得自1986年以来在飞行指导和控制研究所(IFF)中推动了在飞行重食中的研究计划。IFF在IFF上的空气重食计划的重点是对远程测量技术的开发,改进和应用。对于空气传播重食来提高准确性和分辨率,特别重要。另外,IFF使用惯性平台,重力传感器,气压传感器和运动差分载体相位的GPS定位涉及重力测量系统的开发。空气传播的重量法是惯性飞行测量技术的重要组成部分。使用惯性导航系统来测量重力场的原理可以在[1],[2],[3]中找到。重力扰动信号可以从精确惯性加速度计信号(重力传感器)和高度计信号(GPS差分载波相位,气压传感器)之间的时间同步差异获得。重力传感器测量特定力,其由重力分量和飞机加速度分量组成。全球定位系统(GPS)仅测量飞机运动。在[4]中描述了大地和固体地球地球物理学,海洋学和勘探地球物理学中用户的准确性要求。在1公里和10公里之间的波长范围内为0.5mgAt至1mgal的精度是对油勘探的特殊兴趣,在10km到100公里之间的波长为1 mgal至3 mgal的白色对大地度非常重要。

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