Ground Control Considerations for Remotely Piloted Spacecraft
To augment the capabilities of the space transportation system, NASA has funded studies aimed at developing a reusable, remotely piloted spacecraft capable of delivering and retrieving payloads at altitudes and inclinations beyond the reach of the present Shuttle Orbiters. Development of such a remotely piloted spacecraft involves five major categories of human factors design issues related to controllability: 1) mission conditions including thruster plume impingements and signal time delays; 2) vehicle performance variables including control authority, control harmony, minimum impulse, and cross coupling of accelerations; 3) maneuvering task requirements such as target distance and dynamics; 4) control parameters including various control modes and rate/displacement deadbands; and 5) display parameters involving camera placement and function, visual aids, and presentation of operational feedback from the spacecraft. To resolve these human factors design issues, the Martin Marietta Company is presently engaged in a program of research based on high fidelity simulations of remotely piloted spacecraft operations. Preliminary results of these studies will be presented in an interactive session at the 1984 Human Factors Society Annual Convention.